Best Paper - Propulsion and Energy Group
Best Papers in a specific propulsion or energy discipline are selected from papers presented at technical forums by the respective technical committee.
Award Recipients
2025
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Prof Christopher S GoldensteinPurdue UniversityAwarded-CoRecipientsAward: 2023 AIAA Solid Rockets Best PaperAIAA Citation: Dual-Zone Temperature and Multi-Species Measurements in Solid-Propellant Flames via Broadband Mid-Infrared Laser Absorption Spectroscopy AIAA 2023-4029
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Vishnu RadhakrishnaSandia National LaboratoriesAwarded-CoRecipientsAward: 2023 AIAA Solid Rockets Best PaperAIAA Citation: Dual-Zone Temperature and Multi-Species Measurements in Solid-Propellant Flames via Broadband Mid-Infrared Laser Absorption Spectroscopy AIAA 2023-4029
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Prof Steven F SonPurdue UniversityAwarded-CoRecipientsAward: 2023 AIAA Solid Rockets Best PaperAIAA Citation: Dual-Zone Temperature and Multi-Species Measurements in Solid-Propellant Flames via Broadband Mid-Infrared Laser Absorption Spectroscopy AIAA 2023-4029
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Kyle E UhlenhakePurdue UniversityAwarded-CoRecipientsAward: 2023 AIAA Solid Rockets Best PaperAIAA Citation: Dual-Zone Temperature and Multi-Species Measurements in Solid-Propellant Flames via Broadband Mid-Infrared Laser Absorption Spectroscopy AIAA 2023-4029
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Dr Vivek AhujaRESEARCH IN FLIGHTAwarded-CoRecipientsAward: 2023 AIAA Solid Rockets Best Student Paper AwardAIAA Citation: Solid Rocket Motor Internal Ballistics Using a Vortex Particle Method AIAA 2023-4032
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Griffin A DiMaggioAwarded-CoRecipientsAward: 2023 AIAA Solid Rockets Best Student Paper AwardAIAA Citation: Solid Rocket Motor Internal Ballistics Using a Vortex Particle Method AIAA 2023-4032
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Roy J Hartfield JrAuburn UniversityAwarded-CoRecipientsAward: 2023 AIAA Solid Rockets Best Student Paper AwardAIAA Citation: Solid Rocket Motor Internal Ballistics Using a Vortex Particle Method AIAA 2023-4032
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Mr Chris N TorreTorre Space and Power SystemsAwarded-CoRecipientsAward: 2024 AIAA Aerospace Power Systems Best PaperAIAA Citation: Test Performance Results of a Magnetohydrodynamic Generator System Using an Ionized Plasma Flow to Simulate the Interplanetary Solar Wind AIAA 2024-0472
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William V TorreTorre Space and Power Systems LLCAwarded-CoRecipientsAward: 2024 AIAA Aerospace Power Systems Best PaperAIAA Citation: Test Performance Results of a Magnetohydrodynamic Generator System Using an Ionized Plasma Flow to Simulate the Interplanetary Solar Wind AIAA 2024-0472
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Dr Troy HendersonEmbry-Riddle Aeronautical UniversityAwarded-CoRecipientsAward: 2024 AIAA Aerospace Power Systems Best Student PaperAIAA Citation: Power System Testing and Verification for a Space Camera System With 18650 Batteries AIAA 2024-0021
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Daniel PosadaEmbry-Riddle Aeronautical UniversityAwarded-CoRecipientsAward: 2024 AIAA Aerospace Power Systems Best Student PaperAIAA Citation: Power System Testing and Verification for a Space Camera System With 18650 Batteries AIAA 2024-0021
2024
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Madison G AllenNAAwarded-CoRecipientsAward: 2023 AIAA Electric Propulsion Best PaperAIAA Citation: Operation and Performance of a Magnetically Shielded Hall Thruster at Ultrahigh Current Densities on Xenon and Krypton AIAA 2023-0842
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Mr Matthew ByrnePEPLAwarded-CoRecipientsAward: 2023 AIAA Electric Propulsion Best PaperAIAA Citation: Operation and Performance of a Magnetically Shielded Hall Thruster at Ultrahigh Current Densities on Xenon and Krypton AIAA 2023-0842
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Tate GillUniversity of Michigan, Ann ArborAwarded-CoRecipientsAward: 2023 AIAA Electric Propulsion Best PaperAIAA Citation: Operation and Performance of a Magnetically Shielded Hall Thruster at Ultrahigh Current Densities on Xenon and Krypton AIAA 2023-0842
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William HurleyUniversity of MichiganAwarded-CoRecipientsAward: 2023 AIAA Electric Propulsion Best PaperAIAA Citation: Operation and Performance of a Magnetically Shielded Hall Thruster at Ultrahigh Current Densities on Xenon and Krypton AIAA 2023-0842
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Prof Benjamin JornsUniversity of Michigan, Ann ArborAwarded-CoRecipientsAward: 2023 AIAA Electric Propulsion Best PaperAIAA Citation: Operation and Performance of a Magnetically Shielded Hall Thruster at Ultrahigh Current Densities on Xenon and Krypton AIAA 2023-0842
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Mr Thomas A MarksUniversity of Michigan, Ann ArborAwarded-CoRecipientsAward: 2023 AIAA Electric Propulsion Best PaperAIAA Citation: Operation and Performance of a Magnetically Shielded Hall Thruster at Ultrahigh Current Densities on Xenon and Krypton AIAA 2023-0842
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Parker J RobertsUniversity of Michigan, Ann ArborAwarded-CoRecipientsAward: 2023 AIAA Electric Propulsion Best PaperAIAA Citation: Operation and Performance of a Magnetically Shielded Hall Thruster at Ultrahigh Current Densities on Xenon and Krypton AIAA 2023-0842
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Mr Christopher L SercelAwarded-CoRecipientsAward: 2023 AIAA Electric Propulsion Best PaperAIAA Citation: Operation and Performance of a Magnetically Shielded Hall Thruster at Ultrahigh Current Densities on Xenon and Krypton AIAA 2023-0842
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Ms Leanne L SuUniversity of MichiganAwarded-CoRecipientsAward: 2023 AIAA Electric Propulsion Best PaperAIAA Citation: Operation and Performance of a Magnetically Shielded Hall Thruster at Ultrahigh Current Densities on Xenon and Krypton AIAA 2023-0842
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Mr Eric VigesUniversity of Michigan, Ann ArborAwarded-CoRecipientsAward: 2023 AIAA Electric Propulsion Best PaperAIAA Citation: Operation and Performance of a Magnetically Shielded Hall Thruster at Ultrahigh Current Densities on Xenon and Krypton AIAA 2023-0842
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Mr Collin B WhittakerUniversity of MichiganAwarded-CoRecipientsAward: 2023 AIAA Electric Propulsion Best PaperAIAA Citation: Operation and Performance of a Magnetically Shielded Hall Thruster at Ultrahigh Current Densities on Xenon and Krypton AIAA 2023-0842
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Dr John P ClarkAFRLAwarded-CoRecipientsAward: 2023 AIAA Gas Turbine Engines Best PaperAIAA Citation: High-Lift High-Work LPT Blades and Separation: A Machine-Learning-Based Approach to Separation Identification AIAA 2023-0113
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Nathan FletcherInnovative Scientific Solutions, Inc.Awarded-CoRecipientsAward: 2023 AIAA Gas Turbine Engines Best PaperAIAA Citation: High-Lift High-Work LPT Blades and Separation: A Machine-Learning-Based Approach to Separation Identification AIAA 2023-0113
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Mr Jared N KerestesWright State UniversityAwarded-CoRecipientsAward: 2023 AIAA Gas Turbine Engines Best PaperAIAA Citation: High-Lift High-Work LPT Blades and Separation: A Machine-Learning-Based Approach to Separation Identification AIAA 2023-0113
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Dr Christopher R MarksAir Force Research LaboratoryAwarded-CoRecipientsAward: 2023 AIAA Gas Turbine Engines Best PaperAIAA Citation: High-Lift High-Work LPT Blades and Separation: A Machine-Learning-Based Approach to Separation Identification AIAA 2023-0113
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Dr Mitch WolffWright State UniversityAwarded-CoRecipientsAward: 2023 AIAA Gas Turbine Engines Best PaperAIAA Citation: High-Lift High-Work LPT Blades and Separation: A Machine-Learning-Based Approach to Separation Identification AIAA 2023-0113
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Esteban Cisneros-GaribayPrinceton UniversityAwarded-CoRecipientsAward: 2023 AIAA High Speed Air Breathing Propulsion Best PaperAIAA Citation: Manifold-based Modeling for Supersonic Turbulent Combustion AIAA 2023-2529
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Dr Datta V GaitondeThe Ohio State UniversityAwarded-CoRecipientsAward: 2023 AIAA Inlets, Nozzles, and Propulsion System Integration Best PaperAIAA Citation: Modal Analysis of Serpentine Diffuser Distortion AIAA 2023-3308
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Dr Russell W PowersNaval Air Warfare CenterAwarded-CoRecipientsAward: 2023 AIAA Inlets, Nozzles, and Propulsion System Integration Best PaperAIAA Citation: Modal Analysis of Serpentine Diffuser Distortion AIAA 2023-3308
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Dr John T SpyropoulosNAVAIRAwarded-CoRecipientsAward: 2023 AIAA Inlets, Nozzles, and Propulsion System Integration Best PaperAIAA Citation: Modal Analysis of Serpentine Diffuser Distortion AIAA 2023-3308
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Mr Spencer L StahlAwarded-CoRecipientsAward: 2023 AIAA Inlets, Nozzles, and Propulsion System Integration Best PaperAIAA Citation: Modal Analysis of Serpentine Diffuser Distortion AIAA 2023-3308
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Mr Wolfgang ArmbrusterDLR-German Aerospace CenterAwarded-CoRecipientsAward: 2023 AIAA Liquid Propulsion Best PaperAIAA Citation: Flame-Acoustic Interaction in a Sub- and Supercritical, Single-Injector, LOX/CNG/LNG Rocket Combustor with Optical Access AIAA 2023-1838
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Dr Justin HardiDLR Institute of Space PropulsionAwarded-CoRecipientsAward: 2023 AIAA Liquid Propulsion Best PaperAIAA Citation: Flame-Acoustic Interaction in a Sub- and Supercritical, Single-Injector, LOX/CNG/LNG Rocket Combustor with Optical Access AIAA 2023-1838
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Jan MartinDLRAwarded-CoRecipientsAward: 2023 AIAA Liquid Propulsion Best PaperAIAA Citation: Flame-Acoustic Interaction in a Sub- and Supercritical, Single-Injector, LOX/CNG/LNG Rocket Combustor with Optical Access AIAA 2023-1838
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Dr Eric BachTU BerlinAwarded-CoRecipientsAward: 2023 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Low-Order Model for Detonation Velocity Suppression in Rotating Detonation Combustors AIAA 2023-1291
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Miss Provence BarnouinTU BerlinAwarded-CoRecipientsAward: 2023 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Low-Order Model for Detonation Velocity Suppression in Rotating Detonation Combustors AIAA 2023-1291
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Dr Myles BohonTechnische Universität BerlinAwarded-CoRecipientsAward: 2023 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Low-Order Model for Detonation Velocity Suppression in Rotating Detonation Combustors AIAA 2023-1291
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Prof Ephraim J GutmarkUniversity of CincinnatiAwarded-CoRecipientsAward: 2023 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Low-Order Model for Detonation Velocity Suppression in Rotating Detonation Combustors AIAA 2023-1291
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Prof Christian O PaschereitTechnische Universität BerlinAwarded-CoRecipientsAward: 2023 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Low-Order Model for Detonation Velocity Suppression in Rotating Detonation Combustors AIAA 2023-1291
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Marco AdornoPolitecnico di TorinoAwarded-CoRecipientsAward: 2023 AIAA Solid Rockets Best PaperAIAA Citation: Qualification of HCl in Solid Propellant Combustion Products AIAA 2023-1515
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Dr Stefania CarlottiPolitecnico di MilanoAwarded-CoRecipientsAward: 2023 AIAA Solid Rockets Best PaperAIAA Citation: Qualification of HCl in Solid Propellant Combustion Products AIAA 2023-1515
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Stefano DossiPolitecnico Di MilanoAwarded-CoRecipientsAward: 2023 AIAA Solid Rockets Best PaperAIAA Citation: Qualification of HCl in Solid Propellant Combustion Products AIAA 2023-1515
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Andrea GalavottiSPLabAwarded-CoRecipientsAward: 2023 AIAA Solid Rockets Best PaperAIAA Citation: Qualification of HCl in Solid Propellant Combustion Products AIAA 2023-1515
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Dr Filippo MaggiPolitecnico Di MilanoAwarded-CoRecipientsAward: 2023 AIAA Solid Rockets Best PaperAIAA Citation: Qualification of HCl in Solid Propellant Combustion Products AIAA 2023-1515
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Dr Arianna MasiniHomeAwarded-CoRecipientsAward: 2023 AIAA Solid Rockets Best PaperAIAA Citation: Qualification of HCl in Solid Propellant Combustion Products AIAA 2023-1515
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Dr Agostino NeriEuropean Space Agency (ESA)Awarded-CoRecipientsAward: 2023 AIAA Solid Rockets Best PaperAIAA Citation: Qualification of HCl in Solid Propellant Combustion Products AIAA 2023-1515
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Mr Luca NicheliniPolitecnico di MilanoAwarded-CoRecipientsAward: 2023 AIAA Solid Rockets Best PaperAIAA Citation: Qualification of HCl in Solid Propellant Combustion Products AIAA 2023-1515
2023
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Prof Daniele BianchiSapienza University of RomeAwarded-CoRecipientsAward: 2021 AIAA Hybrid Rockets Best PaperAIAA Citation: Machine Learning Techniques for Flight Performance Prediction of Hybrid Rocket Engines AIAA 2021-3506
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Mr Lorenzo FedericiAwarded-CoRecipientsAward: 2021 AIAA Hybrid Rockets Best PaperAIAA Citation: Machine Learning Techniques for Flight Performance Prediction of Hybrid Rocket Engines AIAA 2021-3506
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Dr Mario Tindaro MigliorinoSapienza University of RomeAwarded-CoRecipientsAward: 2021 AIAA Hybrid Rockets Best PaperAIAA Citation: Machine Learning Techniques for Flight Performance Prediction of Hybrid Rocket Engines AIAA 2021-3506
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Dr Alessandro ZavoliSapienza University of RomeAwarded-CoRecipientsAward: 2021 AIAA Hybrid Rockets Best PaperAIAA Citation: Machine Learning Techniques for Flight Performance Prediction of Hybrid Rocket Engines AIAA 2021-3506
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Paolo ZollaLa SapienzaAwarded-CoRecipientsAward: 2021 AIAA Hybrid Rockets Best PaperAIAA Citation: Machine Learning Techniques for Flight Performance Prediction of Hybrid Rocket Engines AIAA 2021-3506
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Fabio A BendanaAwarded-CoRecipientsAward: 2021 AIAA Hybrid Rockets Best Student PaperAIAA Citation: Swirl injection in hybrid PMMA combustion assessed by thermochemical imaging AIAA 2021-3513
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Ms Isabelle C SandersUCLAAwarded-CoRecipientsAward: 2021 AIAA Hybrid Rockets Best Student PaperAIAA Citation: Swirl injection in hybrid PMMA combustion assessed by thermochemical imaging AIAA 2021-3513
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Mr Kevin SchwarmUCLAAwarded-CoRecipientsAward: 2021 AIAA Hybrid Rockets Best Student PaperAIAA Citation: Swirl injection in hybrid PMMA combustion assessed by thermochemical imaging AIAA 2021-3513
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Dr Raymond Mitchell SpearrinUniversity of California Los AngelesAwarded-CoRecipientsAward: 2021 AIAA Hybrid Rockets Best Student PaperAIAA Citation: Swirl injection in hybrid PMMA combustion assessed by thermochemical imaging AIAA 2021-3513
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Nora G. StacyUniversity of California Los AngelesAwarded-CoRecipientsAward: 2021 AIAA Hybrid Rockets Best Student PaperAIAA Citation: Swirl injection in hybrid PMMA combustion assessed by thermochemical imaging AIAA 2021-3513
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Alexander FeleoAwarded-CoRecipientsAward: 2021 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Effects of Inlet Area Ratio on Operability of an Axial Air Inlet Rotating Detonation Combustor AIAA 2021-3676
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Dr Mirko GambaUniversity of MichiganAwarded-CoRecipientsAward: 2021 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Effects of Inlet Area Ratio on Operability of an Axial Air Inlet Rotating Detonation Combustor AIAA 2021-3676
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Joshua ShepardUniversity of MichiganAwarded-CoRecipientsAward: 2021 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Effects of Inlet Area Ratio on Operability of an Axial Air Inlet Rotating Detonation Combustor AIAA 2021-3676
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Dr Brian T BojkoNaval Research LaboratoryAwarded-CoRecipientsAward: 2021 AIAA Propellants and Combustion Best PaperAIAA Citation: Modeling of Layered Ammonium Perchlorate Composite Propellant with Different Burning Rates AIAA 2021-1970
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Monique McClainPurdue UniversityAwarded-CoRecipientsAward: 2021 AIAA Propellants and Combustion Best PaperAIAA Citation: Modeling of Layered Ammonium Perchlorate Composite Propellant with Different Burning Rates AIAA 2021-1970
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Simon RayAwarded-CoRecipientsAward: 2021 AIAA Propellants and Combustion Best PaperAIAA Citation: Modeling of Layered Ammonium Perchlorate Composite Propellant with Different Burning Rates - AIAA 2021-1970
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Dr Vernon H ChaplinJet Propulsion Laboratory (JPL)Awarded-CoRecipientsAward: 2022 AIAA Electric Propulsion Best PaperAIAA Citation: Experimental Characterization of Wave-Induced Azimuthal Ion Velocities in a Hollow Cathode Plume AIAA 2022-1561
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Prof Benjamin JornsUniversity of Michigan, Ann ArborAwarded-CoRecipientsAward: 2022 AIAA Electric Propulsion Best PaperAIAA Citation: Experimental Characterization of Wave-Induced Azimuthal Ion Velocities in a Hollow Cathode Plume AIAA 2022-1561
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Parker J RobertsUniversity of Michigan, Ann ArborAwarded-CoRecipientsAward: 2022 AIAA Electric Propulsion Best PaperAIAA Citation: Experimental Characterization of Wave-Induced Azimuthal Ion Velocities in a Hollow Cathode Plume AIAA 2022-1561
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Linkai LiNAUUAwarded-CoRecipientsAward: 2022 AIAA Gas Turbine Engine Best PaperAIAA Citation: An Experimental Study on the Dynamic Ice Accretion Process over the Surfaces of the Rotating Fan Blades of an Aero-Engine Model - AIAA 2022-2435
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Dr Linchuan TianAwarded-CoRecipientsAward: 2022 AIAA Gas Turbine Engine Best PaperAIAA Citation: An Experimental Study on the Dynamic Ice Accretion Process over the Surfaces of the Rotating Fan Blades of an Aero-Engine Model - AIAA 2022-2435
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Prof Hyungrok DoSeoul National UniversityAwarded-CoRecipientsAward: 2022 AIAA High Speed Air Breathing Propulsion Best PaperAIAA Citation: From Thermal Choking to Inlet Buzz of Circular Scramjets in High-Enthalpy Flows AIAA 2022-0202
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Mr Kyungrae KangSeoul National UniversityAwarded-CoRecipientsAward: 2022 AIAA High Speed Air Breathing Propulsion Best PaperAIAA Citation: From Thermal Choking to Inlet Buzz of Circular Scramjets in High-Enthalpy Flows AIAA 2022-0202
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Dr Qili LiuPurdue UniversityAwarded-CoRecipientsAward: 2022 AIAA High Speed Air Breathing Propulsion Best PaperAIAA Citation: From Thermal Choking to Inlet Buzz of Circular Scramjets in High-Enthalpy Flows AIAA 2022-0202
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Prof Li QiaoSchool of Aeronautics & Astronautics, Purdue UniversityAwarded-CoRecipientsAward: 2022 AIAA High Speed Air Breathing Propulsion Best PaperAIAA Citation: From Thermal Choking to Inlet Buzz of Circular Scramjets in High-Enthalpy Flows AIAA 2022-0202
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Lt Col Darrell S CroweAir Force Institute of TechnologyAwarded-CoRecipientsAward: 2022 AIAA Inlets Nozzles and Propulsion System Integration Best PaperAIAA Citation: Summary of the 5th Propulsion Aerodynamics Workshop Nozzle Test Case: Heated Nozzle Exhaust Passing Over a Flim-cooled Plate AIAA 2022-0086
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Dr Nicholas J GeorgiadisNASA Glenn Research CenterAwarded-CoRecipientsAward: 2022 AIAA Inlets Nozzles and Propulsion System Integration Best PaperAIAA Citation: Summary of the 5th Propulsion Aerodynamics Workshop Nozzle Test Case: Heated Nozzle Exhaust Passing Over a Flim-cooled Plate AIAA 2022-0086
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Kristen Karman-ShoemakeCadence Design Systems, Inc.Awarded-CoRecipientsAward: 2022 AIAA Inlets Nozzles and Propulsion System Integration Best PaperAIAA Citation: Summary of the 5th Propulsion Aerodynamics Workshop Nozzle Test Case: Heated Nozzle Exhaust Passing Over a Flim-cooled Plate AIAA 2022-0086
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Dr Mark P WernetNASA Glenn Research CenterAwarded-CoRecipientsAward: 2022 AIAA Inlets Nozzles and Propulsion System Integration Best PaperAIAA Citation: Summary of the 5th Propulsion Aerodynamics Workshop Nozzle Test Case: Heated Nozzle Exhaust Passing Over a Flim-cooled Plate AIAA 2022-0086
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Dr Chad M WinklerThe Boeing CompanyAwarded-CoRecipientsAward: 2022 AIAA Inlets Nozzles and Propulsion System Integration Best PaperAIAA Citation: Summary of the 5th Propulsion Aerodynamics Workshop Nozzle Test Case: Heated Nozzle Exhaust Passing Over a Flim-cooled Plate AIAA 2022-0086
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Ms Carolyn WoeberCadence Design Systems, Inc.Awarded-CoRecipientsAward: 2022 AIAA Inlets Nozzles and Propulsion System Integration Best PaperAIAA Citation: Summary of the 5th Propulsion Aerodynamics Workshop Nozzle Test Case: Heated Nozzle Exhaust Passing Over a Flim-cooled Plate AIAA 2022-0086
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Subodh AdhikariAwarded-CoRecipientsAward: 2022 AIAA Joint Liquid Propulsion and Propellants and Combustion Best Paper AwardAIAA Citation: Simultaneous OH, CH2O and flow field imaging of near blowoff dynamics AIAA-2022-2348
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Dr Benjamin L Emerson IIAwarded-CoRecipientsAward: 2022 AIAA Joint Liquid Propulsion and Propellants and Combustion Best Paper AwardAIAA Citation: Simultaneous OH, CH2O and flow field imaging of near blowoff dynamics AIAA-2022-2348
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Dr Christopher Allen FuggerSpectral Energies, LLCAwarded-CoRecipientsAward: 2022 AIAA Joint Liquid Propulsion and Propellants and Combustion Best Paper AwardAIAA Citation: Simultaneous OH, CH2O and flow field imaging of near blowoff dynamics AIAA-2022-2348
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Prof Tim C LieuwenGeorgia Institute of TechnologyAwarded-CoRecipientsAward: 2022 AIAA Joint Liquid Propulsion and Propellants and Combustion Best Paper AwardAIAA Citation: Simultaneous OH, CH2O and flow field imaging of near blowoff dynamics AIAA-2022-2348
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Raghul Manosh KumarGeorgia Institute of TechnologyAwarded-CoRecipientsAward: 2022 AIAA Joint Liquid Propulsion and Propellants and Combustion Best Paper AwardAIAA Citation: Simultaneous OH, CH2O and flow field imaging of near blowoff dynamics AIAA-2022-2348
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Valentin BuyakofuNagoya UniversityAwarded-CoRecipientsAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Dr Ikkoh FunakiJapan Aerospace Exploration AgencyAwarded-CoRecipientsAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Keisuke GotoNagoya UniversityAwarded-CoRecipientsAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Prof Hiroto HabuJapan Aerospace Exploration AgencyAwarded-CoRecipientsAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Mr Kazuki IshiharaNagoya UniversityAwarded-CoRecipientsAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Dr Noboru ItouyamaNagoya UniversityAwarded-CoRecipientsAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Akira KawasakiAwarded-CoRecipientsAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Prof Ken MatsuokaNagoya UniversityAwarded-CoRecipientsAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Mr Koichi MatsuyamaIMaSS, Nagoya UniversityAwarded-CoRecipientsAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Mr Tatsuro NakaoJapan Aerospace Exploration Agency (JAXA))Awarded-CoRecipientsAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Dr Daisuke NakataMuroran Institute of TechnologyAwarded-CoRecipientsAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Prof Steven F SonPurdue UniversityAwarded-CoRecipientsAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Modeling of Layered Ammonium Perchlorate Composite Propellant with Different Burning Rates - AIAA 2021-1970
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Dr Shinsuke TakeuchiJapan Aerospace Exploration AgencyAwarded-CoRecipientsAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Dr Masaharu UchiumiJapan Aerospace Exploration AgencyAwarded-CoRecipientsAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Dr Hiroaki WatanabeCRIEPIAwarded-CoRecipientsAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Dr Kazuhiko YamadaJapan Aerospace Exploration AgencyAwarded-CoRecipientsAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
2022
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Jason KirkAwarded-CoRecipientsAward: 1AIAA Citation: Results for an Electrified Aircraft Propulsion Design Exploration AIAA-2021-3280
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Dr Stephen A DanczykAFRL - Air Force Research LaboratoryAwarded-CoRecipientsAward: 2020 AIAA Pressure Gain Combustion Best Paper AwardAIAA Citation: MHz Mid-infrared Laser Absorption of CO and CO2 for Pressure, Temperature, and Species in Rotating Detonation Rocket Flows AIAA-2020-3867
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Dr William A Hargus JrUSAF/AFRL/RQRCAwarded-CoRecipientsAward: 2020 AIAA Pressure Gain Combustion Best Paper AwardAIAA Citation: MHz Mid-infrared Laser Absorption of CO and CO2 for Pressure, Temperature, and Species in Rotating Detonation Rocket Flows AIAA-2020-3867
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Dr Jason Michael KrieselOpto-Knowledge Systems IncAwarded-CoRecipientsAward: 2020 AIAA Pressure Gain Combustion Best Paper AwardAIAA Citation: MHz Mid-infrared Laser Absorption of CO and CO2 for Pressure, Temperature, and Species in Rotating Detonation Rocket Flows AIAA-2020-3867
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Daniel D LeeAwarded-CoRecipientsAward: 2020 AIAA Pressure Gain Combustion Best Paper AwardAIAA Citation: MHz Mid-infrared Laser Absorption of CO and CO2 for Pressure, Temperature, and Species in Rotating Detonation Rocket Flows AIAA-2020-3867
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Anil P NairUniversity of California - Los AngelesAwarded-CoRecipientsAward: 2020 AIAA Pressure Gain Combustion Best Paper AwardAIAA Citation: MHz Mid-infrared Laser Absorption of CO and CO2 for Pressure, Temperature, and Species in Rotating Detonation Rocket Flows AIAA-2020-3867
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Daniel I PinedaAwarded-CoRecipientsAward: 2020 AIAA Pressure Gain Combustion Best Paper AwardAIAA Citation: MHz Mid-infrared Laser Absorption of CO and CO2 for Pressure, Temperature, and Species in Rotating Detonation Rocket Flows AIAA-2020-3867
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Tate GillUniversity of Michigan, Ann ArborAwarded-CoRecipientsAward: 2021 AIAA Electric Propulsion Best Paper AwardAIAA Citation: Performance Measurements of a 5 kW-Class Rotating Magnetic Field Thruster AIAA 2021-3384
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Prof Benjamin JornsUniversity of Michigan, Ann ArborAwarded-CoRecipientsAward: 2021 AIAA Electric Propulsion Best Paper AwardAIAA Citation: Performance Measurements of a 5 kW-Class Rotating Magnetic Field Thruster AIAA 2021-3384
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Mr Christopher L SercelAwarded-CoRecipientsAward: 2021 AIAA Electric Propulsion Best Paper AwardAIAA Citation: Performance Measurements of a 5 kW-Class Rotating Magnetic Field Thruster AIAA 2021-3384
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Joshua M WoodsUniversity of MichiganAwarded-CoRecipientsAward: 2021 AIAA Electric Propulsion Best Paper AwardAIAA Citation: Performance Measurements of a 5 kW-Class Rotating Magnetic Field Thruster AIAA 2021-3384
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Dr Nathaniel J BlaesserNASA Langley Research CenterAwarded-CoRecipientsAward: 2021 AIAA Electrified Aircraft Technology Best Paper AwardAIAA Citation: Results for an Electrified Aircraft Propulsion Design Exploration AIAA-2021-3280
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Kenneth L FisherNASA-Glenn Research CenterAwarded-CoRecipientsAward: 2021 AIAA Electrified Aircraft Technology Best Paper AwardAIAA Citation: Results for an Electrified Aircraft Propulsion Design Exploration AIAA-2021-3280
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Mr Peter C FredericAwarded-CoRecipientsAward: 2021 AIAA Electrified Aircraft Technology Best Paper AwardAIAA Citation: Results for an Electrified Aircraft Propulsion Design Exploration AIAA-2021-3280
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Mr Zachary J FrederickNASA Langley Research CenterAwarded-CoRecipientsAward: 2021 AIAA Electrified Aircraft Technology Best Paper AwardAIAA Citation: Results for an Electrified Aircraft Propulsion Design Exploration AIAA-2021-3280
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Mark D GuynnNASA Langley Research CenterAwarded-CoRecipientsAward: 2021 AIAA Electrified Aircraft Technology Best Paper AwardAIAA Citation: Results for an Electrified Aircraft Propulsion Design Exploration AIAA-2021-3280
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Mr Ty MarienNASA Langley Research CenterAwarded-CoRecipientsAward: 2021 AIAA Electrified Aircraft Technology Best Paper AwardAIAA Citation: Results for an Electrified Aircraft Propulsion Design Exploration AIAA-2021-3280
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Dr Steven J SchneiderNASA Glenn Research CenterAwarded-CoRecipientsAward: 2021 AIAA Electrified Aircraft Technology Best Paper AwardAIAA Citation: Results for an Electrified Aircraft Propulsion Design Exploration AIAA-2021-3280
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Robert P ThackerNASA Glenn Research CenterAwarded-CoRecipientsAward: 2021 AIAA Electrified Aircraft Technology Best Paper AwardAIAA Citation: Results for an Electrified Aircraft Propulsion Design Exploration AIAA-2021-3280
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Dr Aaron H AuslenderNASA Langley Research CenterAwarded-CoRecipientsAward: 2021 AIAA High Speed Air Breathing Propulsion Best Paper AwardAIAA Citation: Application of Flux-Conserved Modeling to an Unsteady Combustion Driven Pseudo-Shock AIAA-2021-1763
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Dr Jeffrey M DonbarUSAFAwarded-CoRecipientsAward: 2021 AIAA High Speed Air Breathing Propulsion Best Paper AwardAIAA Citation: Application of Flux-Conserved Modeling to an Unsteady Combustion Driven Pseudo-Shock AIAA-2021-1763
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Mr Louis M EdelmanNASA Langley Research CenterAwarded-CoRecipientsAward: 2021 AIAA High Speed Air Breathing Propulsion Best Paper AwardAIAA Citation: Application of Flux-Conserved Modeling to an Unsteady Combustion Driven Pseudo-Shock AIAA-2021-1763
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Dr Mirko GambaUniversity of MichiganAwarded-CoRecipientsAward: 2021 AIAA High Speed Air Breathing Propulsion Best Paper AwardAIAA Citation: Application of Flux-Conserved Modeling to an Unsteady Combustion Driven Pseudo-Shock AIAA-2021-1763
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Mark A HagenmaierAir Force Reseach LaboratoryAwarded-CoRecipientsAward: 2021 AIAA High Speed Air Breathing Propulsion Best Paper AwardAIAA Citation: Application of Flux-Conserved Modeling to an Unsteady Combustion Driven Pseudo-Shock AIAA-2021-1763
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Robin HuntNASA Langley Research CenterAwarded-CoRecipientsAward: 2021 AIAA High Speed Air Breathing Propulsion Best Paper AwardAIAA Citation: Application of Flux-Conserved Modeling to an Unsteady Combustion Driven Pseudo-Shock AIAA-2021-1763
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Alicia Benhidjeb-CarayonJet Propulsion Laboratory (JPL)Awarded-CoRecipientsAward: 2021 AIAA Liquid Propulsion Best Paper AwardAIAA Citation: Chemical Composition of Mixed Oxides of Nitrogen using Raman Spectroscopy AIAA-2021-3589
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Victoria M BoulosAwarded-CoRecipientsAward: 2021 AIAA Liquid Propulsion Best Paper AwardAIAA Citation: Chemical Composition of Mixed Oxides of Nitrogen using Raman Spectroscopy AIAA-2021-3589
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Mr Jason R GablAwarded-CoRecipientsAward: 2021 AIAA Liquid Propulsion Best Paper AwardAIAA Citation: Chemical Composition of Mixed Oxides of Nitrogen using Raman Spectroscopy AIAA-2021-3589
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Robin OrthUSAFAwarded-CoRecipientsAward: 2021 AIAA Liquid Propulsion Best Paper AwardAIAA Citation: Chemical Composition of Mixed Oxides of Nitrogen using Raman Spectroscopy AIAA-2021-3589
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Dr Timothee L PourpointPurdue UniversityAwarded-CoRecipientsAward: 2021 AIAA Liquid Propulsion Best Paper AwardAIAA Citation: Chemical Composition of Mixed Oxides of Nitrogen using Raman Spectroscopy AIAA-2021-3589
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Ms Catriona WhiteIndiana University - Purdue University at IndianapolisAwarded-CoRecipientsAward: 2021 AIAA Liquid Propulsion Best Paper AwardAIAA Citation: Chemical Composition of Mixed Oxides of Nitrogen using Raman Spectroscopy AIAA-2021-3589
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Dr Donald H FergusonNational Energy Technology LaboratoryAwarded-CoRecipientsAward: 2021 AIAA Pressure Gain Combustion Best Paper AwardAIAA Citation: Individual Wave Detection and Tracking within a Rotating Detonation Engine through Computer Vision Object Detection applied to High-Speed Images AIAA-2021-1382
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Kristyn JohnsonWest Virginia UniversityAwarded-CoRecipientsAward: 2021 AIAA Pressure Gain Combustion Best Paper AwardAIAA Citation: Individual Wave Detection and Tracking within a Rotating Detonation Engine through Computer Vision Object Detection applied to High-Speed Images AIAA-2021-1382
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Dr Andrew C NixWest Virginia UniversityAwarded-CoRecipientsAward: 2021 AIAA Pressure Gain Combustion Best Paper AwardAIAA Citation: Individual Wave Detection and Tracking within a Rotating Detonation Engine through Computer Vision Object Detection applied to High-Speed Images AIAA-2021-1382
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Prof Matteo BernardiniSapienza University of RomeAwarded-CoRecipientsAward: 2021 AIAA Solid Rockets Best Paper AwardAIAA Citation: Implicit Large-Eddy Simulation of Solid Rocket Motors using the Immersed Boundary Method AIAA-2021-3696
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Dr Enrico CavalliniAgenzia Spaziale ItalianaAwarded-CoRecipientsAward: 2021 AIAA Solid Rockets Best Paper AwardAIAA Citation: Implicit Large-Eddy Simulation of Solid Rocket Motors using the Immersed Boundary Method AIAA-2021-3696
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Mr Matteo CiminiSapienza University of RomeAwarded-CoRecipientsAward: 2021 AIAA Solid Rockets Best Paper AwardAIAA Citation: Implicit Large-Eddy Simulation of Solid Rocket Motors using the Immersed Boundary Method AIAA-2021-3696
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Mr. Andrea Di MascioINSEANAwarded-CoRecipientsAward: 2021 AIAA Solid Rockets Best Paper AwardAIAA Citation: Implicit Large-Eddy Simulation of Solid Rocket Motors using the Immersed Boundary Method AIAA-2021-3696
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Dr Emanuele MartelliSecond University of NaplesAwarded-CoRecipientsAward: 2021 AIAA Solid Rockets Best Paper AwardAIAA Citation: Implicit Large-Eddy Simulation of Solid Rocket Motors using the Immersed Boundary Method AIAA-2021-3696
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Dr Francesco SalvadoreCINECAAwarded-CoRecipientsAward: 2021 AIAA Solid Rockets Best Paper AwardAIAA Citation: Implicit Large-Eddy Simulation of Solid Rocket Motors using the Immersed Boundary Method AIAA-2021-3696
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Prof Fulvio StellaSapienza University of RomeAwarded-CoRecipientsAward: 2021 AIAA Solid Rockets Best Paper AwardAIAA Citation: Implicit Large-Eddy Simulation of Solid Rocket Motors using the Immersed Boundary Method AIAA-2021-3696
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Haiyang HuIowa State UniversityAwarded-CoRecipientsAward: 2022 AIAA Gas Turbine Engine Best PaperAIAA Citation: An Experimental Study on the Dynamic Ice Accretion Process over the Surfaces of the Rotating Fan Blades of an Aero-Engine Model - AIAA 2022-2435
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Prof Jiro KasaharaNagoya UniversityAwarded-CoRecipientsAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Dr Vivek AhujaAwarded-CoRecipientsAward: 2022 AIAA Solid Rockets Best Paper AwardAIAA Citation: Solid Rocket Motor Internal Ballistics with a Surface-Vorticity Solver AIAA-2022-1898
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Griffin A DiMaggioAwarded-CoRecipientsAward: 2022 AIAA Solid Rockets Best Paper AwardAIAA Citation: Solid Rocket Motor Internal Ballistics with a Surface-Vorticity Solver AIAA-2022-1898
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Roy J Hartfield JrAuburn UniversityAwarded-CoRecipientsAward: 2022 AIAA Solid Rockets Best Paper AwardAIAA Citation: Solid Rocket Motor Internal Ballistics with a Surface-Vorticity Solver AIAA-2022-1898
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Prof Joseph MajdalaniAuburn UniversityAwarded-CoRecipientsAward: 2022 AIAA Solid Rockets Best Paper AwardAIAA Citation: Solid Rocket Motor Internal Ballistics with a Surface-Vorticity Solver AIAA-2022-1898
2021
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Mr Jeffryes W ChapmanNASAAwardedAward: 2020 AIAA Electric Aircraft Technology Best Paper AwardAIAA Citation: A Study of Large Scale Power Extraction and Insertion on Turbofan Performance and Stability AIAA-2020-3547
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Dr Ethan Thomas DaleUniversity of Michigan, Ann ArborAwarded-CoRecipientsAward: 2020 AIAA Electric Propulsion Best PaperAIAA Citation: A Predictive Hall Thruster Model Enabled by Data-Driven Closure AIAA-2020-3622
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Prof Benjamin JornsUniversity of Michigan, Ann ArborAwarded-CoRecipientsAward: 2020 AIAA Electric Propulsion Best PaperAIAA Citation: A Predictive Hall Thruster Model Enabled by Data-Driven Closure AIAA-2020-3622
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Mr Thomas A MarksUniversity of Michigan, Ann ArborAwarded-CoRecipientsAward: 2020 AIAA Electric Propulsion Best PaperAIAA Citation: A Predictive Hall Thruster Model Enabled by Data-Driven Closure AIAA-2020-3622
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Dr Lien C YangSelfAwardedAward: 2020 AIAA Energetic Components and Systems Best PaperAIAA Citation: New Formulation for Studying of Detonation Of Gaseous Energetic Mixtures II: CH4/O2 & CH4/Air AIAA-2020-3653
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Dr Gregory J HuntWilliam & MaryAwarded-CoRecipientsAward: 2020 AIAA High Speed Air Breathing Propulsion Best Paper AwardAIAA Citation: Adaptive Pressure Profile Method to Locate the Isolator Shock Train Leading Edge Given Limited Pressure Information AIAA-2020-3715
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Robin HuntNASA Langley Research CenterAwarded-CoRecipientsAward: 2020 AIAA High Speed Air Breathing Propulsion Best Paper AwardAIAA Citation: Adaptive Pressure Profile Method to Locate the Isolator Shock Train Leading Edge Given Limited Pressure Information AIAA-2020-3715
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Dr Damiano BaccarellaUniversity of TennesseeAwarded-CoRecipientsAward: 2020 AIAA High Speed Air Breathing Propulsion Best Professional PaperAIAA Citation: "Flow Choking Induced by Combustion and Mass Injection in a Circular Model Scramjet at Mach 4.5" (AIAA-2020-1611)
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Gyu Sub LeeUniversity of Illinois at Urbana-ChampaignAwarded-CoRecipientsAward: 2020 AIAA High Speed Air Breathing Propulsion Best Professional PaperAIAA Citation: "Flow Choking Induced by Combustion and Mass Injection in a Circular Model Scramjet at Mach 4.5" (AIAA-2020-1611)
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Dr Tonghun LeeUniversity of Illinois at Urbana ChampaignAwarded-CoRecipientsAward: 2020 AIAA High Speed Air Breathing Propulsion Best Professional PaperAIAA Citation: "Flow Choking Induced by Combustion and Mass Injection in a Circular Model Scramjet at Mach 4.5" (AIAA-2020-1611)
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Dr Qili LiuUniversity of Illinois at Urbana-ChampaignAwarded-CoRecipientsAward: 2020 AIAA High Speed Air Breathing Propulsion Best Professional PaperAIAA Citation: "Flow Choking Induced by Combustion and Mass Injection in a Circular Model Scramjet at Mach 4.5" (AIAA-2020-1611)
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Dr Elizabeth T JensJet Propulsion Laboratory (JPL)Awarded-CoRecipientsAward: 2020 AIAA Hybrid Rockets Best PaperAIAA Citation: Combustion Efficiency in Single Port Hybrid Rocket Engines AIAA-2020-3746
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Dr Ashley C KarpJet Propulsion Laboratory (JPL)Awarded-CoRecipientsAward: 2020 AIAA Hybrid Rockets Best PaperAIAA Citation: Combustion Efficiency in Single Port Hybrid Rocket Engines AIAA-2020-3746
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George T StoryNASA Marshall Space Flight CenterAwarded-CoRecipientsAward: 2020 AIAA Hybrid Rockets Best PaperAIAA Citation: Combustion Efficiency in Single Port Hybrid Rocket Engines AIAA-2020-3746
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Mr George R WhittinghillWhittinghill Aerospace LLCAwarded-CoRecipientsAward: 2020 AIAA Hybrid Rockets Best PaperAIAA Citation: Combustion Efficiency in Single Port Hybrid Rocket Engines AIAA-2020-3746
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Mr Mehmet KahramanAwarded-CoRecipientsAward: 2020 AIAA Hybrid Rockets Best Student PaperAIAA Citation: Enhancement of Fuel Regression Rate for Hybrid Rockets by Introducing Novel Coaxial Tube Injector AIAA-2020-3733
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Dr Arif M KarabeyogluSpace Propulsion Group, Inc.Awarded-CoRecipientsAward: 2020 AIAA Hybrid Rockets Best Student PaperAIAA Citation: Enhancement of Fuel Regression Rate for Hybrid Rockets by Introducing Novel Coaxial Tube Injector AIAA-2020-3733
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Mr. Ibrahim OzkalIstanbul Techinal UniversityAwarded-CoRecipientsAward: 2020 AIAA Hybrid Rockets Best Student PaperAIAA Citation: Enhancement of Fuel Regression Rate for Hybrid Rockets by Introducing Novel Coaxial Tube Injector AIAA-2020-3733
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ENS David L EllisNASA Glenn Research CenterAwarded-CoRecipientsAward: 2020 AIAA Liquid Propulsion Best PaperAIAA Citation: Lightweight Thrust Chamber Assemblies using Multi-Alloy Additive Manufacturing and Composite Overwrap AIAA-2020-3787
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John C FikesFD02Awarded-CoRecipientsAward: 2020 AIAA Liquid Propulsion Best PaperAIAA Citation: Lightweight Thrust Chamber Assemblies using Multi-Alloy Additive Manufacturing and Composite Overwrap AIAA-2020-3787
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Paul R GradlNASA Marshall Space Flight CenterAwarded-CoRecipientsAward: 2020 AIAA Liquid Propulsion Best PaperAIAA Citation: Lightweight Thrust Chamber Assemblies using Multi-Alloy Additive Manufacturing and Composite Overwrap AIAA-2020-3787
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Dr Tyler B HudsonNASA Langley Research CenterAwarded-CoRecipientsAward: 2020 AIAA Liquid Propulsion Best PaperAIAA Citation: Lightweight Thrust Chamber Assemblies using Multi-Alloy Additive Manufacturing and Composite Overwrap AIAA-2020-3787
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Mr. Sandi G MillerNASA Glenn Research CenterAwarded-CoRecipientsAward: 2020 AIAA Liquid Propulsion Best PaperAIAA Citation: Lightweight Thrust Chamber Assemblies using Multi-Alloy Additive Manufacturing and Composite Overwrap AIAA-2020-3787
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Christopher S ProtzNASA Marshall Space Flight CenterAwarded-CoRecipientsAward: 2020 AIAA Liquid Propulsion Best PaperAIAA Citation: Lightweight Thrust Chamber Assemblies using Multi-Alloy Additive Manufacturing and Composite Overwrap AIAA-2020-3787
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Dr Geoffrey A LandisNASA Glenn Research CenterAwarded-CoRecipientsAward: 2020 AIAA Power and Energy Forum Best PaperAIAA Citation: 2020 Propulsion and Energy Forum Power Generation from Interplanetary and Interstellar Plasma and Magnetic Fields
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Matt Wentzel-LongNASA Glenn Research CenterAwarded-CoRecipientsAward: 2020 AIAA Power and Energy Forum Best PaperAIAA Citation: 2020 Propulsion and Energy Forum Power Generation from Interplanetary and Interstellar Plasma and Magnetic Fields
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Dr Robert B AdamsNASA Marshall Space Flight CenterAwarded-CoRecipientsAward: 2020 AIAA Power and Energy Forum Best Student PaperAIAA Citation: Elements of an Inductive Electrical Power Conversion System for Fusion-Class Plasmas AIAA-2020-3539
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Jason T CassibryAwarded-CoRecipientsAward: 2020 AIAA Power and Energy Forum Best Student PaperAIAA Citation: Elements of an Inductive Electrical Power Conversion System for Fusion-Class Plasmas AIAA-2020-3539
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Nathan SchillingAwarded-CoRecipientsAward: 2020 AIAA Power and Energy Forum Best Student PaperAIAA Citation: Elements of an Inductive Electrical Power Conversion System for Fusion-Class Plasmas AIAA-2020-3539
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Mr Eric BachTU BerlinAwarded-CoRecipientsAward: 2020 AIAA Pressure Gain Combustion Best Professional PaperAIAA Citation: "RDC Operation and Performance with Varying Air Injector Pressure Loss" (AIAA-2020-0199)
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Prof Christian O PaschereitTechnical University of BerlinAwarded-CoRecipientsAward: 2020 AIAA Pressure Gain Combustion Best Professional PaperAIAA Citation: "RDC Operation and Performance with Varying Air Injector Pressure Loss" (AIAA-2020-0199)
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Prof Panagiotis StathopoulosAwarded-CoRecipientsAward: 2020 AIAA Pressure Gain Combustion Best Professional PaperAIAA Citation: "RDC Operation and Performance with Varying Air Injector Pressure Loss: (AIAA-2020-0199)
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Dr Charlotte DebusDLR - German Aerospace CenterAwarded-CoRecipientsAward: 2020 AIAA Propellants and Combustion Best PaperAIAA Citation: High-performance data analytics of hybrid rocket fuel combustion data using different machine learning approaches AIAA-2020-1161
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Dr Mario KobaldDLR-German Aerospace CenterAwarded-CoRecipientsAward: 2020 AIAA Propellants and Combustion Best PaperAIAA Citation: High-performance data analytics of hybrid rocket fuel combustion data using different machine learning approaches AIAA-2020-1161
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Ms Anna PetraroloDLR LampoldshausenAwarded-CoRecipientsAward: 2020 AIAA Propellants and Combustion Best PaperAIAA Citation: High-performance data analytics of hybrid rocket fuel combustion data using different machine learning approaches AIAA-2020-1161
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Alexander RüttgersInstitute for Software TechnologyAwarded-CoRecipientsAward: 2020 AIAA Propellants and Combustion Best PaperAIAA Citation: High-performance data analytics of hybrid rocket fuel combustion data using different machine learning approaches AIAA-2020-1161
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Dr Martin SiggelDLR - German Aerospace CenterAwarded-CoRecipientsAward: 2020 AIAA Propellants and Combustion Best PaperAIAA Citation: High-performance data analytics of hybrid rocket fuel combustion data using different machine learning approaches AIAA-2020-1161
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Prof Claude Russell Joyner IIAerojet RocketdyneAwarded-CoRecipientsAward: 2020 Nuclear and Future Flight Propulsion Best PaperAIAA Citation: Mars Opposition Missions Using Nuclear Thermal Propulsion AIAA-2020-3850
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Dr Timothy S KokanAerojet RocketdyneAwarded-CoRecipientsAward: 2020 Nuclear and Future Flight Propulsion Best PaperAIAA Citation: Mars Opposition Missions Using Nuclear Thermal Propulsion AIAA-2020-3850
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Daniel J LevackAerojet RocketdyneAwarded-CoRecipientsAward: 2020 Nuclear and Future Flight Propulsion Best PaperAIAA Citation: Mars Opposition Missions Using Nuclear Thermal Propulsion AIAA-2020-3850
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Mr Brian J MuzekAerojet RocketdyneAwarded-CoRecipientsAward: 2020 Nuclear and Future Flight Propulsion Best PaperAIAA Citation: Mars Opposition Missions Using Nuclear Thermal Propulsion AIAA-2020-3850
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Mr Christopher Britton ReynoldsAerojet RocketdyneAwarded-CoRecipientsAward: 2020 Nuclear and Future Flight Propulsion Best PaperAIAA Citation: Mars Opposition Missions Using Nuclear Thermal Propulsion AIAA-2020-3850
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Mr Joseph Kalyan Raj I.TECHNION - ISRAEL INST OF TECHAwarded-CoRecipientsAward: 2020 Power and Energy Forum Best Student PaperAIAA Citation: Development of a Deep Space Nuclear Electric Propulsion (NEP) System - a NuAER Plasma NEP Reactor AIAA-2020-3540
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Mr Joseph Kalyan Raj I.TECHNION - ISRAEL INST OF TECHAwarded-CoRecipientsAward: 2020 Power and Energy Forum Best Student PaperAIAA Citation: Development of a Deep Space Nuclear Electric Propulsion (NEP) System - a NuAER Plasma NEP Reactor AIAA-2020-3540
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Dr Geoff ParksAwarded-CoRecipientsAward: 2020 Power and Energy Forum Best Student PaperAIAA Citation: Development of a Deep Space Nuclear Electric Propulsion (NEP) System - a NuAER Plasma NEP Reactor AIAA-2020-3540
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Mr amaury AWESISAE SupaeroAwarded-CoRecipientsAward: 2021 AIAA Gas Turbine Engines Best PaperAIAA Citation: Unsteady Body Force Methodology for Fan Operability Assessment under Clean and Distorted Inflow Conditions AIAA-2021-0388
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Dr Xavier CarbonneauISAE SUPAEROAwarded-CoRecipientsAward: 2021 AIAA Gas Turbine Engines Best PaperAIAA Citation: Unsteady Body Force Methodology for Fan Operability Assessment under Clean and Distorted Inflow Conditions AIAA-2021-0388
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Dr Julien MartyONERAAwarded-CoRecipientsAward: 2021 AIAA Gas Turbine Engines Best PaperAIAA Citation: Unsteady Body Force Methodology for Fan Operability Assessment under Clean and Distorted Inflow Conditions AIAA-2021-0388
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Dr David Kenneth HallThe Pennsylvania State UniversityAwarded-CoRecipientsAward: 2021 AIAA Inlets Nozzles and Propulsion System Integration Best PaperAIAA Citation: Propulsor Models for Computational Analysis of Aircraft Aerodynamic Performance with Boundary Layer Ingestion AIAA-2021-0991
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Mr Michael K LieuAurora Flight Sciences, A Boeing CompanyAwarded-CoRecipientsAward: 2021 AIAA Inlets Nozzles and Propulsion System Integration Best PaperAIAA Citation: Propulsor Models for Computational Analysis of Aircraft Aerodynamic Performance with Boundary Layer Ingestion AIAA-2021-0991
2020
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Mr John A Brand IIAwarded-CoRecipientsAward: “Comparative Analysis and Justification of Optimal Rocket Motor Selection in NASA USLI by Applying Newton’s Second Law to a Variable Mass Body” (AIAA 2019-4138)
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Dr Trevor S ElliottUniversity of Tennessee at ChattanoogaAwarded-CoRecipientsAward: “Comparative Analysis and Justification of Optimal Rocket Motor Selection in NASA USLI by Applying Newton’s Second Law to a Variable Mass Body” (AIAA 2019-4138)
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Brandon RobertsAwarded-CoRecipientsAward: “Comparative Analysis and Justification of Optimal Rocket Motor Selection in NASA USLI by Applying Newton’s Second Law to a Variable Mass Body” (AIAA 2019-4138)
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Mr Ashwyn Mathew SamAwarded-CoRecipientsAward: “Comparative Analysis and Justification of Optimal Rocket Motor Selection in NASA USLI by Applying Newton’s Second Law to a Variable Mass Body” (AIAA 2019-4138)
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Dr Andreea BocaJet Propulsion LaboratoryAwardedAward: 2019 AIAA Aerospace Power Systems Best Paper AwardAIAA Citation: “Solar Power for Deep-Space Applications: State of Art and Development” (AIAA 2019-4236)
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Robert S KowalczykAwardedAward: 2019 AIAA Aerospace Power Systems Best Paper AwardAIAA Citation: “Solar Power for Deep-Space Applications: State of Art and Development” (AIAA 2019-4236)
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Patrick McClureLos Alamos National LaboratoryAwardedAward: 2019 AIAA Aerospace Power Systems Best Student Paper Competition AwardAIAA Citation: “Hydrogen Loss Effects on Mircoreactors for Space and Planetary Nuclear Power Production” (AIAA 2019-4452)
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Mr Vedant Kiritkumar MehtaAwardedAward: 2019 AIAA Aerospace Power Systems Best Student Paper Competition AwardAIAA Citation: “Hydrogen Loss Effects on Mircoreactors for Space and Planetary Nuclear Power Production” (AIAA 2019-4452)
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Dr Dan M GoebelJet Propulsion LaboratoryAwarded-CoRecipientsAward: 2019 AIAA Electric Propulsion Best Paper AwardAIAA Citation: “High Power Demonstration of a 100 kW Nested Hall Thruster System (AIAA-2019-3809)
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Dr Scott J HallNASA Glenn Research CenterAwarded-CoRecipientsAward: 2019 AIAA Electric Propulsion Best Paper AwardAIAA Citation: “High Power Demonstration of a 100 kW Nested Hall Thruster System (AIAA-2019-3809)
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Dr Richard R HoferJet Propulsion LaboratoryAwarded-CoRecipientsAward: 2019 AIAA Electric Propulsion Best Paper AwardAIAA Citation: “High Power Demonstration of a 100 kW Nested Hall Thruster System (AIAA-2019-3809)
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Prof Benjamin JornsUniversity of Michigan, Ann ArborAwarded-CoRecipientsAward: 2019 AIAA Electric Propulsion Best Paper AwardAIAA Citation: “High Power Demonstration of a 100 kW Nested Hall Thruster System (AIAA-2019-3809)
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Sarah W.H. SharkAerojet RocketdyneAwarded-CoRecipientsAward: 2019 AIAA Electric Propulsion Best Paper AwardAIAA Citation: “High Power Demonstration of a 100 kW Nested Hall Thruster System (AIAA-2019-3809)
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Dr Robert A BaurleNASA-Langley Research CenterAwarded-CoRecipientsAward: 2019 AIAA High Speed Air Breathing Propulsion Best Paper AwardAIAA Citation: “Using Computational Flow Imaging to Optimize Filtered Rayleigh Scattering Measurements of an Isolator Shock Train” (AIAA 2019-4016)
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Dr Paul M DanehyNASA Langley Research CenterAwardedAward: 2019 AIAA High Speed Air Breathing Propulsion Best Paper AwardAIAA Citation: “Using Computational Flow Imaging to Optimize Filtered Rayleigh Scattering Measurements of an Isolator Shock Train” (AIAA 2019-4016)
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Dr Cody Ryan GroundNASA Langley Research CenterAwarded-CoRecipientsAward: 2019 AIAA High Speed Air Breathing Propulsion Best Paper AwardAIAA Citation: “Using Computational Flow Imaging to Optimize Filtered Rayleigh Scattering Measurements of an Isolator Shock Train” (AIAA 2019-4016)
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Robin HuntNASA Langley Research CenterAwarded-CoRecipientsAward: 2019 AIAA High Speed Air Breathing Propulsion Best Paper AwardAIAA Citation: “Using Computational Flow Imaging to Optimize Filtered Rayleigh Scattering Measurements of an Isolator Shock Train” (AIAA 2019-4016)
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Mr Enrico PaccagnellaAwarded-CoRecipientsAward: 2019 AIAA Hybrid Rockets Best Paper AwardAIAA Citation: “Real Time Deep Throttling Tests of a Hydrogen Peroxide Hybrid Rocket Motor” (AIAA 2019-4266)
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Daniele PavarinUniversity of PadovaAwarded-CoRecipientsAward: 2019 AIAA Hybrid Rockets Best Paper AwardAIAA Citation: “Real Time Deep Throttling Tests of a Hydrogen Peroxide Hybrid Rocket Motor” (AIAA 2019-4266)
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Eur Ing Francesco BaratoCISAS-University of PadovaAwarded-CoRecipientsAward: 2019 AIAA Hybrid Rockets Best Paper AwardAIAA Citation: “Real Time Deep Throttling Tests of a Hydrogen Peroxide Hybrid Rocket Motor” (AIAA 2019-4266)
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Marco SantiAwarded-CoRecipientsAward: 2019 AIAA Hybrid Rockets Best Paper AwardAIAA Citation: “Real Time Deep Throttling Tests of a Hydrogen Peroxide Hybrid Rocket Motor” (AIAA 2019-4266)
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Dr Brian J CantwellStanford UniversityAwarded-CoRecipientsAward: 2019 AIAA Hybrid Rockets Best Student Paper AwardAIAA Citation: “Experimental Findings on Pre- and Post-combustion Chamber Effects in a Laboratory-scale motor” (AIAA 2019-4336)
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Flora S MechentelAwarded-CoRecipientsAward: 2019 AIAA Hybrid Rockets Best Student Paper AwardAIAA Citation: “Experimental Findings on Pre- and Post-combustion Chamber Effects in a Laboratory-scale motor” (AIAA 2019-4336)
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Matthew D LangfordTechsburg IncAwarded-CoRecipientsAward: 2019 AIAA Inlets, Nozzles, and Propulsion System Integration Best Paper AwaAIAA Citation: “Development of a Ducted Propulsor for BLI Electric Regional Aircraft – Part I: Aerodynamic Design and Analysis” (AIAA-2019-3853)
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Mr Cory CombsAmpaire Inc.Awarded-CoRecipientsAward: 2019 AIAA Inlets, Nozzles, and Propulsion System Integration Best Paper AwardAIAA Citation: “Development of a Ducted Propulsor for BLI Electric Regional Aircraft – Part I: Aerodynamic Design and Analysis” (AIAA-2019-3853)
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Dr Jonathan L FlemingTechsburgAwarded-CoRecipientsAward: 2019 AIAA Inlets, Nozzles, and Propulsion System Integration Best Paper AwardAIAA Citation: “Development of a Ducted Propulsor for BLI Electric Regional Aircraft – Part I: Aerodynamic Design and Analysis” (AIAA-2019-3853)
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Dr WingFai NgTechsburg, Inc.Awarded-CoRecipientsAward: 2019 AIAA Inlets, Nozzles, and Propulsion System Integration Best Paper AwardAIAA Citation: “Development of a Ducted Propulsor for BLI Electric Regional Aircraft – Part I: Aerodynamic Design and Analysis” (AIAA-2019-3853)
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Dr Kenneth A BrownSandia National LaboratoriesAwarded-CoRecipientsAward: 2019 AIAA Inlets, Nozzles, and Propulsion System Integration Best Paper Award fromAIAA Citation: “Development of a Ducted Propulsor for BLI Electric Regional Aircraft – Part I: Aerodynamic Design and Analysis” (AIAA-2019-3853)
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Paul R GradlNASA Marshall Space Flight CenterAwarded-CoRecipientsAward: 2019 AIAA Liquid Propulsion Best PaperAIAA Citation: “Additive Manufacturing and Hot-fire Testing of Liquid Rocket Channel Wall Nozzles Using Blown Powder Directed Energy Deposition Inconel 625 and JBK-75 Alloys” (AIAA-2019-4362)
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Dr Christopher S ProtzNASAAwarded-CoRecipientsAward: 2019 AIAA Liquid Propulsion Best Paper AwardAIAA Citation: “Additive Manufacturing and Hot-fire Testing of Liquid Rocket Channel Wall Nozzles Using Blown Powder Directed Energy Deposition Inconel 625 and JBK-75 Alloys” (AIAA-2019-4362)
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Tal WammenNASA Marshall Space Flight CenterAwarded-CoRecipientsAward: 2019 AIAA Liquid Propulsion Best Paper AwardAIAA Citation: “Additive Manufacturing and Hot-fire Testing of Liquid Rocket Channel Wall Nozzles Using Blown Powder Directed Energy Deposition Inconel 625 and JBK-75 Alloys” (AIAA-2019-4362)
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Prof Claude Russell Joyner IIAerojet RocketdyneAwarded-CoRecipientsAward: 2019 AIAA Nuclear and Future Flight Best Paper AwardAIAA Citation: “Applications of Nuclear Thermal Propulsion to Lunar Architectures” (AIAA 2019-4032)
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Dr Timothy S KokanAerojet RocketdyneAwarded-CoRecipientsAward: 2019 AIAA Nuclear and Future Flight Best Paper AwardAIAA Citation: “Applications of Nuclear Thermal Propulsion to Lunar Architectures” (AIAA 2019-4032)
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Daniel J LevackAerojet RocketdyneAwarded-CoRecipientsAward: 2019 AIAA Nuclear and Future Flight Best Paper AwardAIAA Citation: “Applications of Nuclear Thermal Propulsion to Lunar Architectures” (AIAA 2019-4032)
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Mr Christopher Britton ReynoldsAerojet RocketdyneAwarded-CoRecipientsAward: 2019 AIAA Nuclear and Future Flight Best Paper AwardAIAA Citation: “Applications of Nuclear Thermal Propulsion to Lunar Architectures” (AIAA 2019-4032)
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Arin E. L. CrossAwarded-CoRecipientsAward: 2019 AIAA Propellants and Combustion Best Paper AwardAIAA Citation: “Influence of Cross-Frequency Interactions on Nonstationary Thermoacoustic Oscillations in a Rich-Burn Gas Turbine Combustor at Elevated Pressure” (AIAA-2019-3949)
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Mitchell L PassarelliGeorgia Institute of TechnologyAwarded-CoRecipientsAward: 2019 AIAA Propellants and Combustion Best Paper AwardAIAA Citation: “Influence of Cross-Frequency Interactions on Nonstationary Thermoacoustic Oscillations in a Rich-Burn Gas Turbine Combustor at Elevated Pressure” (AIAA-2019-3949)
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Prof Adam M SteinbergGeorgia Institute of TechnologyAwarded-CoRecipientsAward: 2019 AIAA Propellants and Combustion Best Paper AwardAIAA Citation: “Influence of Cross-Frequency Interactions on Nonstationary Thermoacoustic Oscillations in a Rich-Burn Gas Turbine Combustor at Elevated Pressure” (AIAA-2019-3949)
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Dr Krishna VenkatesanGE Global Research CenterAwardedAward: 2019 AIAA Propellants and Combustion Best Paper AwardAIAA Citation: “Influence of Cross-Frequency Interactions on Nonstationary Thermoacoustic Oscillations in a Rich-Burn Gas Turbine Combustor at Elevated Pressure” (AIAA-2019-3949)
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Mr Austin P MurrayAwarded-CoRecipientsAward: 2019 AIAA Propulsion Education Best Student Paper AwardAIAA Citation: “Development and Experimentation of a Lab-Scale Pulse Detonation Engine (PDE)” (AIAA 2019-3808)
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Dr Jeffrey D MoorePenn State AltoonaAwarded-CoRecipientsAward: 2019 AIAA Propulsion Education Best Student Paper AwardAIAA Citation: “Development and Experimentation of a Lab-Scale Pulse Detonation Engine (PDE)” (AIAA 2019-3808)
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Eric PittmanAwarded-CoRecipientsAward: 2019 AIAA Propulsion Education Best Student Paper AwardAIAA Citation: “Development and Experimentation of a Lab-Scale Pulse Detonation Engine (PDE)” (AIAA 2019-3808)
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Mr Tyler L Smith IAwarded-CoRecipientsAward: 2019 AIAA Propulsion Education Best Student Paper AwardAIAA Citation: “Development and Experimentation of a Lab-Scale Pulse Detonation Engine (PDE)” (AIAA 2019-3808)
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Kennethe G CooperNASA Marshall Space Flight CenterAwarded-CoRecipientsAward: 2019 ASME Aerospace Division Propulsion Technical Committee Best Paper AwardAIAA Citation: “GRCop-42 Development and Hot-fire Testing Using Additive Manufacturing Powder Bed Fusion for Channel-Cooled Combustion Chambers” (AIAA 2019-4228)
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Paul R GradlNASA Marshall Space Flight CenterAwarded-CoRecipientsAward: 2019 ASME Aerospace Division Propulsion Technical Committee Best Paper AwardAIAA Citation: “GRCop-42 Development and Hot-fire Testing Using Additive Manufacturing Powder Bed Fusion for Channel-Cooled Combustion Chambers” (AIAA 2019-4228)
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Dr Christopher S ProtzNASAAwarded-CoRecipientsAward: 2019 ASME Aerospace Division Propulsion Technical Committee Best Paper AwardAIAA Citation: “GRCop-42 Development and Hot-fire Testing Using Additive Manufacturing Powder Bed Fusion for Channel-Cooled Combustion Chambers” (AIAA 2019-4228)
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ENS David L EllisNASA Glenn Research CenterAwarded-CoRecipientsAward: 2019 ASME Aerospace Division Propulsion Technical Committee Best Paper AwardAIAA Citation: “GRCop-42 Development and Hot-fire Testing Using Additive Manufacturing Powder Bed Fusion for Channel-Cooled Combustion Chambers” (AIAA 2019-4228)
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Laura EvansNASA Glenn Research CenterAwarded-CoRecipientsAward: 2019 ASME Aerospace Division Propulsion Technical Committee Best Paper AwardAIAA Citation: “GRCop-42 Development and Hot-fire Testing Using Additive Manufacturing Powder Bed Fusion for Channel-Cooled Combustion Chambers” (AIAA 2019-4228)
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Chance P GarciaAwarded-CoRecipientsAward: 2019 ASME Aerospace Division Propulsion Technical Committee Best Paper AwardAIAA Citation: “GRCop-42 Development and Hot-fire Testing Using Additive Manufacturing Powder Bed Fusion for Channel-Cooled Combustion Chambers” (AIAA 2019-4228)
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Dr Ali A AmeriNASA Glenn Research CenterAwarded-CoRecipientsAward: 2020 AIAA Gas Turbine Engines Best Paper AwardAIAA Citation: “Conjugate Heat Transfer Study of Innovative Pin-Fin Cooling Configuration ” (AIAA-2020-0634)
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Dr Jeffrey P BonsOhio State UniversityAwarded-CoRecipientsAward: 2020 AIAA Gas Turbine Engines Best Paper AwardAIAA Citation: “Conjugate Heat Transfer Study of Innovative Pin-Fin Cooling Configuration ” (AIAA-2020-0634)
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Fabian ChaconAwarded-CoRecipientsAward: Study of Parasitic Combustion in an Optically Accessible Continuous Wave Rotating Detonation Engine (AIAA 2019-0473)AIAA Citation: 2019 AIAA High Speed Air Breathing Propulsion Best Paper
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Alessandro RuffinAwarded-CoRecipientsAward: the 2019 AIAA Hybrid Rockets Best Paper AwardAIAA Citation: “Real Time Deep Throttling Tests of a Hydrogen Peroxide Hybrid Rocket Motor” (AIAA 2019-4266)
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Dr Timothy M WabelAwarded-CoRecipientsAward: the 2019 AIAA Propellants and Combustion Best Paper AwardAIAA Citation: “Influence of Cross-Frequency Interactions on Nonstationary Thermoacoustic Oscillations in a Rich-Burn Gas Turbine Combustor at Elevated Pressure” (AIAA-2019-3949)
2019
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Dr Vlad J HrubyBusek Co, Inc.Awarded-CoRecipientsAward: 2018 Electric Propulsion Best PaperAIAA Citation: “In-Flight Verification and Validation of Colloid Microthruster Performance” (AIAA 2018-4643)
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Dr Noel T ClemensThe University of Texas at AustinAwarded-CoRecipientsAward: 2019 HSABP Best PaperAIAA Citation: “Supersonic Isolator Shock-Train Dynamics: Simple Physics-Based Model for Closed Loop Control of Shock Train Location” (AIAA 2018-1618
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Dr Leon VanstoneUniversity of Texas at AustinAwarded-CoRecipientsAward: 2019 HSABP Best PaperAIAA Citation: “Supersonic Isolator Shock-Train Dynamics: Simple Physics-Based Model for Closed Loop Control of Shock Train Location” (AIAA 2018-1618
2018
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Jeffreys W. ChapmanNASA Glenn Research Center, Cleveland, OhioAwarded-CoRecipientsAward: "Active Turbine Tip Clearance Control Trade Space Analysis of an Advanced Geared Turbofan Engine"AIAA Citation: AIAA 2018-4822
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Jonathan L. KratzNASA Glenn Research Center, Cleveland, OhioAwarded-CoRecipientsAward: "Active Turbine Tip Clearance Control Trade Space Analysis of an Advanced Geared Turbofan Engine"AIAA Citation: AIAA 2018-4822
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Stany GallierArianeGroup, Vert-le-Petit, FranceAwarded-CoRecipientsAward: "An analytical model for acoustic induced heat release disturbances from aluminum combustion in solid rocket motors"AIAA Citation: AIAA 2018-4788
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Aurélien GenotCNES DLA, Paris, FranceAwarded-CoRecipientsAward: "An analytical model for acoustic induced heat release disturbances from aluminum combustion in solid rocket motors"AIAA Citation: AIAA 2018-4788
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Thierry SchullerLaboratoire EM2C, Toulouse, FranceAwarded-CoRecipientsAward: "An analytical model for acoustic induced heat release disturbances from aluminum combustion in solid rocket motors"AIAA Citation: AIAA 2018-4788
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Marc A. CarboneNASA Glenn Research Center, Cleveland, OhioAwarded-CoRecipientsAward: "An Intelligent Autonomous Power Controller for the NASA Human Deep Space Gateway"AIAA Citation: AIAA-4634
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Jeffrey T. CsankNASA Glenn Research CenterAwarded-CoRecipientsAward: "An Intelligent Autonomous Power Controller for the NASA Human Deep Space Gateway"AIAA Citation: AIAA-4634
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Jeffrey C. FolloNASA Glenn Research Center, Cleveland, OhioAwarded-CoRecipientsAward: "An Intelligent Autonomous Power Controller for the NASA Human Deep Space Gateway"AIAA Citation: AIAA--4634
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Yuhin HauNASA Glenn Reseach Center, Cleveland OhioAwarded-CoRecipientsAward: "An Intelligent Autonomous Power Controller for the NASA Human Deep Space Gateway"AIAA Citation: AIAA-4634
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Matthew J. MuscatelloNASA Glenn Research Center, Cleveland, OhioAwarded-CoRecipientsAward: "An Intelligent Autonomous Power Controller for the NASA Human Deep Space Gateway"AIAA Citation: AIAA-4634
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James F. SoederNASA Glenn Research Center, Cleveland, OhioAwarded-CoRecipientsAward: "An Intelligent Autonomous Power Controller for the NASA Human Deep Space Gateway"AIAA Citation: AIAA-4634
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John W. BennewitzERC, Inc.Awarded-CoRecipientsAward: "Characterization of Detonation Wave Propagation in a Rotating Detonation Rocket Engine using Direct High-Speed Imaging"AIAA Citation: AIAA - 4688
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Blaine R. BiglerERC, Inc.Awarded-CoRecipientsAward: "Characterization of Detonation Wave Propagation in a Rotating Detonation Rocket Engine using Direct High-Speed Imaging"AIAA Citation: AIAA - 4688
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Stephen A. DanczykAir Force Research Laboratory, Wright-Patterson Air Force Base, OHAwarded-CoRecipientsAward: "Characterization of Detonation Wave Propagation in a Rotating Detonation Rocket Engine using Direct High-Speed Imaging"AIAA Citation: AIAA - 4688
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William HargusAir Force Research Laboratory, Wright-Patterson Air Force Base, OHAwarded-CoRecipientsAward: "Characterization of Detonation Wave Propagation in a Rotating Detonation Rocket Engine using Direct High-Speed Imaging"AIAA Citation: AIAA - 4688
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Richard D. SmithGHKN Engineering LLC, Redmond, WashingtonAwarded-CoRecipientsAward: "Characterization of Detonation Wave Propagation in a Rotating Detonation Rocket Engine using Direct High-Speed Imaging"AIAA Citation: AIAA - 4688
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Benjamin L. EmersonSchool of Space Engineering, Georgia Institute of Technology, Atlanta, GeorgiaAwarded-CoRecipientsAward: "Complete Determination of the Velocity Gradient Tensor upstream of the Flame Front with High-Speed Tomo-PIV/Dual-Plane-PIV/OH-PLIF Measurements"AIAA Citation: AIAA - 0153
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Joseph FelverSpectral Energies, LLC, Beavercreek, OhioAwarded-CoRecipientsAward: "Complete Determination of the Velocity Gradient Tensor upstream of the Flame Front with High-Speed Tomo-PIV/Dual-Plane-PIV/OH-PLIF Measurements"AIAA Citation: AIAA - 0153
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Christopher FuggerSpectral Energies, LLC, Beavercreek, OhioAwarded-CoRecipientsAward: "Complete Determination of the Velocity Gradient Tensor upstream of the Flame Front with High-Speed Tomo-PIV/Dual-Plane-PIV/OH-PLIF Measurements"AIAA Citation: AIAA - 0153
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James R. GordAir Force Research Laboratory, Wright-Patterson Air Force Base, OHAwarded-CoRecipientsAward: "Complete Determination of the Velocity Gradient Tensor upstream of the Flame Front with High-Speed Tomo-PIV/Dual-Plane-PIV/OH-PLIF Measurements"AIAA Citation: AIAA - 0153
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Benjamin R. HallsAir Force Research Laboratory, Wright-Patterson Air Force Base, OHAwarded-CoRecipientsAward: "Complete Determination of the Velocity Gradient Tensor upstream of the Flame Front with High-Speed Tomo-PIV/Dual-Plane-PIV/OH-PLIF Measurements"AIAA Citation: AIAA - 0153
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Naibo JiangSpectral Energies, LLC, Beavercreek, OhioAwarded-CoRecipientsAward: "Complete Determination of the Velocity Gradient Tensor upstream of the Flame Front with High-Speed Tomo-PIV/Dual-Plane-PIV/OH-PLIF Measurements"AIAA Citation: AIAA - 0153
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Tim C. LieuwenSchool of Space Engineering, Georgia Institute of Technology, Atlanta, GeorgiaAwarded-CoRecipientsAward: "Complete Determination of the Velocity Gradient Tensor upstream of the Flame Front with High-Speed Tomo-PIV/Dual-Plane-PIV/OH-PLIF Measurements"AIAA Citation: AIAA - 0153
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Jamie LimSchool of Space Engineering, Georgia Institute of Technology, Atlanta, GeorgiaAwarded-CoRecipientsAward: "Complete Determination of the Velocity Gradient Tensor upstream of the Flame Front with High-Speed Tomo-PIV/Dual-Plane-PIV/OH-PLIF Measurements"AIAA Citation: AIAA - 0153
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Sukesh RoySpectral Energies, LLC, Beavercreek, OhioAwarded-CoRecipientsAward: "Complete Determination of the Velocity Gradient Tensor upstream of the Flame Front with High-Speed Tomo-PIV/Dual-Plane-PIV/OH-PLIF Measurements"AIAA Citation: AIAA - 0153
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Matthew SirignanoSchool of Space Engineering, Georgia Institute of Technology, Atlanta, GeorgiaAwarded-CoRecipientsAward: "Complete Determination of the Velocity Gradient Tensor upstream of the Flame Front with High-Speed Tomo-PIV/Dual-Plane-PIV/OH-PLIF Measurements"AIAA Citation: AIAA - 0153
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Mikhail SlipchenkoSpectral Energies, LLC, Beavercreek, OhioAwarded-CoRecipientsAward: "Complete Determination of the Velocity Gradient Tensor upstream of the Flame Front with High-Speed Tomo-PIV/Dual-Plane-PIV/OH-PLIF Measurements"AIAA Citation: AIAA - 0153
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Travis SmithSchool of Space Engineering, Georgia Institute of Technology, Atlanta, GeorgiaAwarded-CoRecipientsAward: "Complete Determination of the Velocity Gradient Tensor upstream of the Flame Front with High-Speed Tomo-PIV/Dual-Plane-PIV/OH-PLIF Measurements"AIAA Citation: AIAA - 0153
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Tongxun YiSpectral Energies, LLC, Beavercreek, OhioAwarded-CoRecipientsAward: "Complete Determination of the Velocity Gradient Tensor upstream of the Flame Front with High-Speed Tomo-PIV/Dual-Plane-PIV/OH-PLIF Measurements"AIAA Citation: AIAA - 0153
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Yu DaimonJapan Aerospace Exploration Agency, Ibaraki, JapanAwarded-CoRecipientsAward: "Computational Analysis of Supercritical and Transcritical Flow in Cooling Channels with Rough Surface"AIAA Citation: AIAA 2018-4465
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Hideto KawashimaJapan Aerospace Exploration Agency, Ibaraki, JapanAwarded-CoRecipientsAward: "Computational Analysis of Supercritical and Transcritical Flow in Cooling Channels with Rough Surface"AIAA Citation: AiAA 2018-4465
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Hideyo NegishiJapan Aerospace Exploration Agency, Ibaraki, JapanAwarded-CoRecipientsAward: "Computational Analysis of Supercritical and Transcritical Flow in Cooling Channels with Rough Surface"AIAA Citation: AIAA 2018-4465
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David L. BlackRetired, Formerly Westinghouse Electric Corporation, Washington, D.C.AwardedAward: "Consideration of Low Enriched Uranium Space Reactors"AIAA Citation: AIAA 2018-4673
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Bhupendra KhandelwalUniversity of Sheffield, Sheffield, South Yorkshire, United KingdomAwarded-CoRecipientsAward: "Impact of alternative fuel on gas turbine noise, vibration and instability"AIAA Citation: AIAA 2019-0240
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Charith J. WijesingheUniversity of Sheffield, Sheffield, South Yorkshire, United KingdomAwarded-CoRecipientsAward: "Impact of alternative fuel on gas turbine noise, vibration and instability"AIAA Citation: AIAA 2019-0240
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Shota HiraiHokkaido University, Sapporo, JapanAwarded-CoRecipientsAward: "Investigation of Graphite Nozzle Erosiion in Hybrid Rockets Using O2/C2H4"AIAA Citation: AIAA 2018-4531
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Landon T. KampsHokkaido University, Sapporo, JapanAwarded-CoRecipientsAward: "Investigation of Graphite Nozzle Erosiion in Hybrid Rockets Using O2/C2H4"AIAA Citation: AIAA 2018-4531
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Naoto AdachiUematsu Electric Co., Akabira, JapanAwarded-CoRecipientsAward: "Investigation of Graphite Nozzle Erosion in Hybrid Rockets Using O2/C2H4"AIAA Citation: AIAA 2018-4531
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Raymond GuanThe University of Alberta, Edmonton, CanadaAwarded-CoRecipientsAward: "Investigation of Graphite Nozzle Erosion in Hybrid Rockets Using O2/C2H4"AIAA Citation: AIAA 2018-4531
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Hikaru IsochiUematsu Electric Co., Akabira, JapanAwarded-CoRecipientsAward: "Investigation of Graphite Nozzle Erosion in Hybrid Rockets Using O2/C2H4"AIAA Citation: AIAA 2018-4531
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Mitsunori ItohIHI Corporation, Yokohama, JapanAwarded-CoRecipientsAward: "Investigation of Graphite Nozzle Erosion in Hybrid Rockets Using O2/C2H4"AIAA Citation: AIAA 2018-4531
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Harunori NagataHokkaido University, Sapporo, JapanAwarded-CoRecipientsAward: "Investigation of Graphite Nozzle Erosion in Hybrid Rockets Using O2/C2H4"AIAA Citation: AIAA 2018-4531
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Yuji SaitoTokoku University, Sendai, JapanAwarded-CoRecipientsAward: "Investigation of Graphite Nozzle Erosion in Hybrid Rockets Using O2/C2H4"AIAA Citation: AIAA 2018-4531
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Kazuhito SakuraiHokkaido University, Sapporo, JapanAwarded-CoRecipientsAward: "Investigation of Graphite Nozzle Erosion in Hybrid Rockets Using O2/C2H4"AIAA Citation: AIAA 2018-4531
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Tor ViscorHokkaido University, Sapporo, JapanAwarded-CoRecipientsAward: "Investigation of Graphite Nozzle Erosion in Hybrid Rockets Using O2/C2H4"AIAA Citation: AIAA 2018-4531
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Toni A. ClarkLeidos, Inc., Reston, VAAwarded-CoRecipientsAward: "Recommendations for Next Generation Crew Quarters"AIAA Citation: ICES 2018-106
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Brandon W. MaryattNASA Johnson Space Center, Houston, TexasAwarded-CoRecipientsAward: "Recommendations for Next Generation Crew Quarters"AIAA Citation: ICES 2018-106
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Michael J. Van WieKBRwyle, Lexington Park, MarylandAwarded-CoRecipientsAward: "Recommendations for Next Generation Crew Quarters"AIAA Citation: ICES 2018-106
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Ronald G. VeraarTNO Defence Security and Safety, Rijswijk, The NetherlandsAwarded-CoRecipientsAward: "Sustained Combustion Limits of a Central Dump Solid Fuel Ramjet Combustor at High Altitude Operational Conditions"AIAA Citation: AIAA 2018-4449
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Wolter WielingTNO Defence Security and Safety, Rijswijk, The NetherlandsAwarded-CoRecipientsAward: "Sustained Combustion Limits of a Central Dump Solid Fuel Ramjet Combustor at High Altitude Operational Conditions"AIAA Citation: AIAA 2018-4449
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Maxwell H. BriggsNASA Glenn Research Center, Cleveland, OhioAwarded-CoRecipientsAward: "The Kilopower Reactor Using Stirling TechnologY (KRUSTY) Nuclear Ground Test Results and Lessons Learned"AIAA Citation: AIAA 2018-4973
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Marc A. GibsonNASA Glenn Research Center, Cleveland, OhioAwarded-CoRecipientsAward: "The Kilopower Reactor Using Stirling TechnologY (KRUSTY) Nuclear Ground Test Results and Lessons Learned"AIAA Citation: AIAA 2018-4973
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Thomas GodfroyVantage Partners, LLC, Brookpark, OhioAwarded-CoRecipientsAward: "The Kilopower Reactor Using Stirling TechnologY (KRUSTY) Nuclear Ground Test Results and Lessons Learned"AIAA Citation: AIAA 2018-4973
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Patrick McClureLos Alamos National Laboratory, Los Alamos, New MexicoAwarded-CoRecipientsAward: "The Kilopower Reactor Using Stirling TechnologY (KRUSTY) Nuclear Ground Test Results and Lessons Learned"AIAA Citation: AIAA 2018-4973
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David I. PostonLos Alamos National Laboratory, Los Alamos, New MexicoAwarded-CoRecipientsAward: "The Kilopower Reactor Using Stirling TechnologY (KRUSTY) Nuclear Ground Test Results and Lessons Learned"AIAA Citation: AIAA 2018-4973
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James I. SanziNASA Glenn Research Center, Cleveland, OhioAwarded-CoRecipientsAward: "The Kilopower Reactor Using Stirling TechnologY (KRUSTY) Nuclear Ground Test Results and Lessons Learned"AIAA Citation: AIAA 2018-4973
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Phil BarelaNASA Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CaliforniaAwarded-CoRecipientsAward: “In-Flight Verification and Validation of Colloid Microthruster Performance”AIAA Citation: AIAA 2018-4643
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Curt CutlerNASA Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CaliforniaAwarded-CoRecipientsAward: “In-Flight Verification and Validation of Colloid Microthruster Performance”AIAA Citation: AIAA 2018-4643
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Nathaniel DemmonsBusek Company, Inc., Natick, MassachusettsAwarded-CoRecipientsAward: “In-Flight Verification and Validation of Colloid Microthruster Performance”AIAA Citation: AIAA 2018-4643
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Charles DunnNASA Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CaliforniaAwarded-CoRecipientsAward: “In-Flight Verification and Validation of Colloid Microthruster Performance”AIAA Citation: AIAA 2018-4643
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Vlad HrubyBusek Company, Inc., Natick, MassachusettsAwarded-CoRecipientsAward: “In-Flight Verification and Validation of Colloid Microthruster Performance”AIAA Citation: AIAA 2018-4643
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Oscar HsuNASA Goddard Space Flight Center, Greenbelt, MarylandAwarded-CoRecipientsAward: “In-Flight Verification and Validation of Colloid Microthruster Performance”AIAA Citation: AIAA 2018-4643
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Shahram JavindaNASA Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CaliforniaAwarded-CoRecipientsAward: “In-Flight Verification and Validation of Colloid Microthruster Performance”AIAA Citation: AIAA 2018-4643
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Thanh LeNASA Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CaliforniaAwarded-CoRecipientsAward: “In-Flight Verification and Validation of Colloid Microthruster Performance”AIAA Citation: AIAA 2018-4643
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Irena LiNASA Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CaliforniaAwarded-CoRecipientsAward: “In-Flight Verification and Validation of Colloid Microthruster Performance”AIAA Citation: AIAA 2018-4643
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Peiman MaghamiNASA Goddard Space Flight Center, Greenbelt, MarylandAwarded-CoRecipientsAward: “In-Flight Verification and Validation of Colloid Microthruster Performance”AIAA Citation: AIAA 2018-4643
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Colleen Marrese-ReadingNASA Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CaliforniaAwarded-CoRecipientsAward: “In-Flight Verification and Validation of Colloid Microthruster Performance”AIAA Citation: AIAA 2018-4643
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James O’DonnellNASA Goddard Space Flight Center, Greenbelt, MarylandAwarded-CoRecipientsAward: “In-Flight Verification and Validation of Colloid Microthruster Performance”AIAA Citation: AIAA 2018-4643
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Andrew Romero-WolfNASA Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CaliforniaAwarded-CoRecipientsAward: “In-Flight Verification and Validation of Colloid Microthruster Performance”AIAA Citation: AIAA 2018-4643
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Jacob SlutskyNASA Goddard Space Flight Center, Greenbelt, MarylandAwarded-CoRecipientsAward: “In-Flight Verification and Validation of Colloid Microthruster Performance”AIAA Citation: AIAA 2018-4643
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James Ira ThorpeNASA Goddard Space Flight Center, Greenbelt, MarylandAwarded-CoRecipientsAward: “In-Flight Verification and Validation of Colloid Microthruster Performance”AIAA Citation: AIAA 2018-4643
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John ZiemerNASA Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CaliforniaAwarded-CoRecipientsAward: “In-Flight Verification and Validation of Colloid Microthruster Performance”AIAA Citation: AIAA 2018-4643
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Mr David WoernerJet Propulsion LaboratoryAwardedAward: 2017 Aerospace Power Systems Best PaperAIAA Citation: Next-Generation RTGs for NASA (AIAA 2017-4612)
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Prof Edgar ChoueiriPrinceton UniversityAwarded-CoRecipientsAward: 2017 Electric Propulsion Best PaperAIAA Citation: choueiri@Princeton.EDU
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William CooganFirefly AerospaceAwarded-CoRecipientsAward: 2017 Electric Propulsion Best PaperAIAA Citation: “A Critical Review of Thrust Models for Applied-Field Magnetoplasmadynamic Thrusters” (AIAA 2017-4723),
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Dr John C Melcher IVNASA-Johnson Space CenterAwarded-CoRecipientsAward: 2017 Liquid Propulsion Best PaperAIAA Citation: "Coil-On-Plug Ignition for Oxygen/Methane Liquid Rocket Engines in Thermal-Vacuum Environments" (AIAA 2017-4666)
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Dr Trevor S ElliottUniversity of Tennessee at ChattanoogaAwarded-CoRecipientsAward: 2017 Solid Rockets Best PaperAIAA Citation: “Biglobal Stability of the Swirling Majdalani-Fist Mean Flowfield in Solid Rocket Motors” (AIAA 2017-4949)
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Mr Wesley A GibsonAwarded-CoRecipientsAward: 2017 Solid Rockets Best PaperAIAA Citation: wes.gibson02@gmail.com
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Mr Dillon P SlussAwarded-CoRecipientsAward: 2017 Solid Rockets Best PaperAIAA Citation: “Biglobal Stability of the Swirling Majdalani-Fist Mean Flowfield in Solid Rocket Motors” (AIAA 2017-4949)
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Dr Carmine CarmicinoUniversità di Napoli Federico IIAwarded-CoRecipientsAward: 2018 Hybrid Rockets Best PaperAIAA Citation: An Analytical Model to Predict Longitudinal Acoustic Modes Frequency of Hybrid Rockets Combustion Chamber (AIAA 2017-4645)
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Prof Dario PastronePolitecnico di TorinoAwarded-CoRecipientsAward: 2018 Hybrid Rockets Best PaperAIAA Citation: An Analytical Model to Predict Longitudinal Acoustic Modes Frequency of Hybrid Rockets Combustion Chamber (AIAA 2017-4645)
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Mr. David J ArendNASA Glenn Research CenterAwarded-CoRecipientsAward: 2018 Inlets, Nozzles, and Propulsion Systems Integration Best PaperAIAA Citation: “Performance Calculations for a Boundary-Layer-Ingesting Fan Stage from Sparse Measurements” (AIAA 2018-1889)
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John A GazzanigaZin Technologies, Inc.Awarded-CoRecipientsAward: 2018 Inlets, Nozzles, and Propulsion Systems Integration Best PaperAIAA Citation: “Performance Calculations for a Boundary-Layer-Ingesting Fan Stage from Sparse Measurements” (AIAA 2018-1889)
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Dr Larry W HardinUnited Technologies Research CenterAwarded-CoRecipientsAward: 2018 Inlets, Nozzles, and Propulsion Systems Integration Best PaperAIAA Citation: “Performance Calculations for a Boundary-Layer-Ingesting Fan Stage from Sparse Measurements” (AIAA 2018-1889)
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Dr Tristan A HearnNASA Glenn Research CenterAwarded-CoRecipientsAward: 2018 Inlets, Nozzles, and Propulsion Systems Integration Best PaperAIAA Citation: “Performance Calculations for a Boundary-Layer-Ingesting Fan Stage from Sparse Measurements” (AIAA 2018-1889)
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Stefanie M HirtNASA Glenn Research CenterAwarded-CoRecipientsAward: 2018 Inlets, Nozzles, and Propulsion Systems Integration Best PaperAIAA Citation: “Performance Calculations for a Boundary-Layer-Ingesting Fan Stage from Sparse Measurements” (AIAA 2018-1889)
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John D WolterNASA Glenn Research CenterAwarded-CoRecipientsAward: 2018 Inlets, Nozzles, and Propulsion Systems Integration Best PaperAIAA Citation: “Performance Calculations for a Boundary-Layer-Ingesting Fan Stage from Sparse Measurements” (AIAA 2018-1889)
2017
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Dr Enrico CavalliniAgenzia Spaziale ItalianaAwarded-CoRecipientsAward: "Motor Scale and Propellant Geometry Effects on Pressure Oscillations in Aft-Finocyl Solid Rocket Motors"AIAA Citation: AIAA 2016-4793
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Dr Agostino NeriEuropean Space Agency (ESA)Awarded-CoRecipientsAward: "Motor Scale and Propellant Geometry Effects on Pressure Oscillations in Aft-Finocyl Solid Rocket Motors"AIAA Citation: AIAA 2016-4793
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Joseph CarneyAwarded-CoRecipientsAward: “Thermal-Mechanical Characterization of Bridgewires and Surrounding Materials Utilizing Thermal Transient Testing”AIAA Citation: AIAA 2016-4932
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Mr. John D GlassAnalex Corporation HeadquartersAwarded-CoRecipientsAward: “Thermal-Mechanical Characterization of Bridgewires and Surrounding Materials Utilizing Thermal Transient Testing”AIAA Citation: AIAA 2016-4932
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Mr Charles J Moore JrNASA Kennedy Space CenterAwarded-CoRecipientsAward: “Thermal-Mechanical Characterization of Bridgewires and Surrounding Materials Utilizing Thermal Transient Testing”AIAA Citation: AIAA 2016-4932
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Dr Luke B RobersonNASA-Kenndey Space CenterAwarded-CoRecipientsAward: “Thermal-Mechanical Characterization of Bridgewires and Surrounding Materials Utilizing Thermal Transient Testing”AIAA Citation: AIAA 2016-4932
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Mr Sebastian OkhovatAwarded-CoRecipientsAward: AIAA 2017-1538, “ The Effect of Pulsed Injection on the Entrainment into a Cavity Based Flameholder in Supersonic Flow,”AIAA Citation: AIAA 2017-1538, “ The Effect of Pulsed Injection on the Entrainment into a Cavity Based Flameholder in Supersonic Flow,”
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Dr Timothy OmbrelloAir Force Research LaboratoryAwarded-CoRecipientsAward: AIAA 2017-1538, “ The Effect of Pulsed Injection on the Entrainment into a Cavity Based Flameholder in Supersonic Flow,”AIAA Citation: AIAA 2017-1538, “ The Effect of Pulsed Injection on the Entrainment into a Cavity Based Flameholder in Supersonic Flow,”
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Dr Leslie A SmithSierra Nevada CorporationAwarded-CoRecipientsAward: AIAA 2017-1538, “ The Effect of Pulsed Injection on the Entrainment into a Cavity Based Flameholder in Supersonic Flow,”AIAA Citation: AIAA 2017-1538, “ The Effect of Pulsed Injection on the Entrainment into a Cavity Based Flameholder in Supersonic Flow,”
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Mr Michael EadesMichael EadesAwarded-CoRecipientsAward: Comparing Low Enriched Fuel to Highly Enriched Fuel for use in Nuclear Thermal Propulsion SystemsAIAA Citation: Comparing Low Enriched Fuel to Highly Enriched Fuel for use in Nuclear Thermal Propulsion Systems
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Prof Claude Russell Joyner IIAerojet RocketdyneAwarded-CoRecipientsAward: Comparing Low Enriched Fuel to Highly Enriched Fuel for use in Nuclear Thermal Propulsion SystemsAIAA Citation: Comparing Low Enriched Fuel to Highly Enriched Fuel for use in Nuclear Thermal Propulsion Systems
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Mr Vishal PatelCenter for Space Nuclear ResearchAwarded-CoRecipientsAward: Comparing Low Enriched Fuel to Highly Enriched Fuel for use in Nuclear Thermal Propulsion SystemsAIAA Citation: Comparing Low Enriched Fuel to Highly Enriched Fuel for use in Nuclear Thermal Propulsion Systems
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Dr Paolo VenneriUSNCAwarded-CoRecipientsAward: Comparing Low Enriched Fuel to Highly Enriched Fuel for use in Nuclear Thermal Propulsion SystemsAIAA Citation: Comparing Low Enriched Fuel to Highly Enriched Fuel for use in Nuclear Thermal Propulsion Systems
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Mrs Samantha J. AlbertsAwarded-CoRecipientsAward: Experiment Design for Measuring Accommodation Coefficients for Modeling of Long-Duration Spaceflight Cryogenic PropellantsAIAA Citation: AIAA 2015-4246
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Prof Steven H CollicottPurdue UniversityAwarded-CoRecipientsAward: Experiment Design for Measuring Accommodation Coefficients for Modeling of Long-Duration Spaceflight Cryogenic PropellantsAIAA Citation: AIAA 2015-4246
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Dr Stephen D HeisterPurdue UniversityAwarded-CoRecipientsAward: Experiment Design for Measuring Accommodation Coefficients for Modeling of Long-Duration Spaceflight Cryogenic PropellantsAIAA Citation: AIAA 2015-4246
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Mr Praveen SrikanthAwarded-CoRecipientsAward: Experiment Design for Measuring Accommodation Coefficients for Modeling of Long-Duration Spaceflight Cryogenic PropellantsAIAA Citation: AIAA 2015-4246
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James F DriscollUniversity of MichiganAwarded-CoRecipientsAward: Experimental Assessment of Premixed Flames Subjected to Extreme TurbulenceAIAA Citation: Experimental Assessment of Premixed Flames Subjected to Extreme Turbulence
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Mr Aaron W SkibaAwarded-CoRecipientsAward: Experimental Assessment of Premixed Flames Subjected to Extreme TurbulenceAIAA Citation: Experimental Assessment of Premixed Flames Subjected to Extreme Turbulence
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Jacob TemmeU. S. Army Research Laboratory (APG)Awarded-CoRecipientsAward: Experimental Assessment of Premixed Flames Subjected to Extreme TurbulenceAIAA Citation: Experimental Assessment of Premixed Flames Subjected to Extreme Turbulence
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Prof Adam P BrucknerAwarded-CoRecipientsAward: Experimental Investigation of a Baffled-Tube Ram AcceleratorAIAA Citation: Experimental Investigation of a Baffled-Tube Ram Accelerator
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Jeffrey F GlusmanAwarded-CoRecipientsAward: Experimental Investigation of a Baffled-Tube Ram AcceleratorAIAA Citation: Experimental Investigation of a Baffled-Tube Ram Accelerator
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Richard D GristAwarded-CoRecipientsAward: Experimental Investigation of a Baffled-Tube Ram AcceleratorAIAA Citation: Experimental Investigation of a Baffled-Tube Ram Accelerator
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Prof Andrew J HigginsMcGill UniversityAwardedAward: Experimental Investigation of a Baffled-Tube Ram AcceleratorAIAA Citation: Experimental Investigation of a Baffled-Tube Ram Accelerator
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Prof Carl KnowlenUniversity of WashingtonAwardedAward: Experimental Investigation of a Baffled-Tube Ram AcceleratorAIAA Citation: Experimental Investigation of a Baffled-Tube Ram Accelerator
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Dr Steven B StanleyAerojet RocketdyneAwarded-CoRecipientsAward: Experimental Investigation of Continuous Detonation Rocket Engines for In-Space Propulsion”AIAA Citation: Experimental Investigation of Continuous Detonation Rocket Engines for In-Space Propulsion”
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Mr Manabu TanakaAwarded-CoRecipientsAward: Fundamental Studies of Radio-Frequency Preionization for Frozen Inert Gas Plasma Magnetohydrodynamic Electric Power GenerationAIAA Citation: Fundamental Studies of Radio-Frequency Preionization for Frozen Inert Gas Plasma Magnetohydrodynamic Electric Power Generation
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Mr James L FelderNASA Glenn Research CenterAwarded-CoRecipientsAward: Installed Performance Assessment of a Boundary Layer Ingesting Distributed Propulsion System at Design PointAIAA Citation: Installed Performance Assessment of a Boundary Layer Ingesting Distributed Propulsion System at Design Point
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Dr Chana GoldbergCranfield UniversityAwarded-CoRecipientsAward: Installed Performance Assessment of a Boundary Layer Ingesting Distributed Propulsion System at Design PointAIAA Citation: Installed Performance Assessment of a Boundary Layer Ingesting Distributed Propulsion System at Design Point
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Dr David G MacManusCranfield UniversityAwarded-CoRecipientsAward: Installed Performance Assessment of a Boundary Layer Ingesting Distributed Propulsion System at Design PointAIAA Citation: Installed Performance Assessment of a Boundary Layer Ingesting Distributed Propulsion System at Design Point
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Dr Devaiah K NaliandaAwarded-CoRecipientsAward: Installed Performance Assessment of a Boundary Layer Ingesting Distributed Propulsion System at Design PointAIAA Citation: Installed Performance Assessment of a Boundary Layer Ingesting Distributed Propulsion System at Design Point
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Pericles PilidisCranfield UniversityAwarded-CoRecipientsAward: Installed Performance Assessment of a Boundary Layer Ingesting Distributed Propulsion System at Design PointAIAA Citation: Installed Performance Assessment of a Boundary Layer Ingesting Distributed Propulsion System at Design Point
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Mr Jasper GrohmannGerman Aerospace Center (DLR)Awarded-CoRecipientsAward: Investigation of differences in lean blowout of liquid single-component fuels in a gas turbine model combustorAIAA Citation: Investigation of differences in lean blowout of liquid single-component fuels in a gas turbine model combustor
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Mr Bastian RauchAwarded-CoRecipientsAward: Investigation of differences in lean blowout of liquid single-component fuels in a gas turbine model combustorAIAA Citation: Investigation of differences in lean blowout of liquid single-component fuels in a gas turbine model combustor
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Dr Ahsan R ChoudhuriUniversity of Texas at El PasoAwarded-CoRecipientsAward: K-12 Minority STEM Education Program: MAA SouthwestAIAA Citation: K-12 Minority STEM Education Program: MAA Southwest
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Mr Michael L EverettUniversity of Texas at El PasoAwarded-CoRecipientsAward: K-12 Minority STEM Education Program: MAA SouthwestAIAA Citation: K-12 Minority STEM Education Program: MAA Southwest
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Dr Norman D Love JrThe University of Texas El PasoAwardedAward: K-12 Minority STEM Education Program: MAA SouthwestAIAA Citation: K-12 Minority STEM Education Program: MAA Southwest
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Mr Maxime BouygesONERAAwarded-CoRecipientsAward: Local Linear Stability Analysis of Non-Circular Injection-Driven Channel FlowsAIAA Citation: AIAA 2016-4701
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Prof Gregoire CasalisONERAAwarded-CoRecipientsAward: Local Linear Stability Analysis of Non-Circular Injection-Driven Channel FlowsAIAA Citation: AIAA 2016-4701
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Mr. Francois ChedevergneENSAE SupaeroAwarded-CoRecipientsAward: Local Linear Stability Analysis of Non-Circular Injection-Driven Channel FlowsAIAA Citation: AIAA 2016-4701
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John R AndersonJet Propulsion LaboratoryAwardedAward: Mechanics for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall ThrusterAIAA Citation: Mechanics for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall Thruster
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Dr Dan M GoebelJet Propulsion LaboratoryAwarded-CoRecipientsAward: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall ThrusterAIAA Citation: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall Thruster
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Christopher A DodsonAwarded-CoRecipientsAward: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall ThrusterAIAA Citation: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall Thruster
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Dr Richard R HoferJet Propulsion LaboratoryAwarded-CoRecipientsAward: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall ThrusterAIAA Citation: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall Thruster
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Dr Alejandro Lopez OrtegaJet Propulsion LaboratoryAwarded-CoRecipientsAward: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall ThrusterAIAA Citation: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall Thruster
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Dr Ioannis G MikellidesJet Propulsion LaboratoryAwarded-CoRecipientsAward: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall ThrusterAIAA Citation: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall Thruster
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Dr Michael J SekerakAwarded-CoRecipientsAward: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall ThrusterAIAA Citation: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall Thruster
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Prof Benjamin JornsUniversity of Michigan, Ann ArborAwardedAward: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall Thruster Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall ThrusterAIAA Citation: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall Thruster Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall Thruster
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Mr Giang Q LamLockheed Martin CorporationAwarded-CoRecipientsAward: Solar Array Design for the Mars InSight Lander MissionAIAA Citation: Solar Array Design for the Mars InSight Lander Mission
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Scott A. BilletsAwarded-CoRecipientsAward: Solar Array Design for the Mars InSight Lander Mission,”AIAA Citation: Solar Array Design for the Mars InSight Lander Mission,”
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Richard W WarwickLockheed Martin Space SystemsAwarded-CoRecipientsAward: Solar Array Design for the Mars InSight Lander Mission,”AIAA Citation: Solar Array Design for the Mars InSight Lander Mission,”
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Stefania CarlottiAwarded-CoRecipientsAward: Vortex Combustion in a Lab-Scale Hybrid Rocket MotorAIAA Citation: AIAA 2016-4562
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Dr Luciano GalfettiPolitecnico di MilanoAwarded-CoRecipientsAward: Vortex Combustion in a Lab-Scale Hybrid Rocket MotorAIAA Citation: AIAA 2016-4562
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Mr Jakub GlowackiAwarded-CoRecipientsAward: Vortex Combustion in a Lab-Scale Hybrid Rocket MotorAIAA Citation: AIAA 2016-4562
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Dr Filippo MaggiPolitecnico Di MilanoAwarded-CoRecipientsAward: Vortex Combustion in a Lab-Scale Hybrid Rocket MotorAIAA Citation: AIAA 2016-4562
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Dr Christian ParavanPolitecnico di MilanoAwarded-CoRecipientsAward: Vortex Combustion in a Lab-Scale Hybrid Rocket MotorAIAA Citation: AIAA 2016-4562
2016
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Dr Olga V KartuzovaNASA Glenn Research CenterAwarded-CoRecipientsAward: "CFD Modeling of the Multipurpose Hydrogen Test Bed (MHTB) Self-Pressurization and Spray Bar Mixing Experiments in Normal Gravity: Effect of the Accommodation Coefficient on the Tank Pressure"AIAA Citation: AIAA 2015-3769
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Dr Mohammad KassemiNASA Glenn Research CenterAwarded-CoRecipientsAward: "CFD Modeling of the Multipurpose Hydrogen Test Bed (MHTB) Self-Pressurization and Spray Bar Mixing Experiments in Normal Gravity: Effect of the Accommodation Coefficient on the Tank Pressure"AIAA Citation: AIAA 2015-3769
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Dr Minel BraunThe University of AkronAwarded-CoRecipientsAward: "Leak Rate Quantification Method for Gas Pressure Seals with Controlled Pressure Differential”AIAA Citation: AIAA 2015-4231
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Dr Christopher C DanielsAwarded-CoRecipientsAward: "Leak Rate Quantification Method for Gas Pressure Seals with Controlled Pressure Differential”AIAA Citation: AIAA 2015-4231
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Dr Heather Ann OravecThe University of AkronAwarded-CoRecipientsAward: "Leak Rate Quantification Method for Gas Pressure Seals with Controlled Pressure Differential”AIAA Citation: AIAA 2015-4231
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Shawn C TaylorNASA Glenn Research CenterAwarded-CoRecipientsAward: "Leak Rate Quantification Method for Gas Pressure Seals with Controlled Pressure Differential”AIAA Citation: AIAA 2015-4231
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Janice WasowskiAwarded-CoRecipientsAward: "Leak Rate Quantification Method for Gas Pressure Seals with Controlled Pressure Differential”AIAA Citation: AIAA 2015-4231
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Michael BeyarBoeing Research & TechnologyAwarded-CoRecipientsAward: "Turbine Powered Simulator Calibration and Testing for Hybrid Wing Body Powered Airframe Integration”AIAA Citation: AIAA 2016-0011
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Jeff D FlammNASA Langley Research CenterAwarded-CoRecipientsAward: "Turbine Powered Simulator Calibration and Testing for Hybrid Wing Body Powered Airframe Integration”AIAA Citation: AIAA 2016-0011
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Kevin D JamesNASA-Ames Research CenterAwarded-CoRecipientsAward: "Turbine Powered Simulator Calibration and Testing for Hybrid Wing Body Powered Airframe Integration”AIAA Citation: AIAA 2016-0011
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Dr Kurtis R LongArc-Aox, Experimental Aerophyscis BranchAwarded-CoRecipientsAward: "Turbine Powered Simulator Calibration and Testing for Hybrid Wing Body Powered Airframe Integration”AIAA Citation: AIAA 2016-0011
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Dr Patrick R SheaNASA Langley Research CenterAwarded-CoRecipientsAward: "Turbine Powered Simulator Calibration and Testing for Hybrid Wing Body Powered Airframe Integration”AIAA Citation: AIAA 2016-0011
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Daniel M TompkinsBoeing Research and TechnologyAwarded-CoRecipientsAward: "Turbine Powered Simulator Calibration and Testing for Hybrid Wing Body Powered Airframe Integration”AIAA Citation: AIAA 2016-0011
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Dr Keith A GonthierLouisiana State UniversityAwarded-CoRecipientsAward: “Analysis of Dissipation Induced by Successive Planar Shock Loading of Granular Explosive”AIAA Citation: AIAA 2015-3708
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Pratap Thamanna RaoLouisiana State UniversityAwarded-CoRecipientsAward: “Analysis of Dissipation Induced by Successive Planar Shock Loading of Granular Explosive”AIAA Citation: AIAA 2015-3708
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Dr Campbell D CarterU.S. Air Force Research LaboratoryAwarded-CoRecipientsAward: “Establishing the Controlling Parameters of Ignition in High-Speed Flow”AIAA Citation: AIAA 2016-0658
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Dr Hyungrok DoUniversity of Notre DameAwarded-CoRecipientsAward: “Establishing the Controlling Parameters of Ignition in High-Speed Flow”AIAA Citation: AIAA 2016-0658
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Dr Ez A HassanAir Force Research LaboratoryAwarded-CoRecipientsAward: “Establishing the Controlling Parameters of Ignition in High-Speed Flow”AIAA Citation: AIAA 2016-0658
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Philip IvancicAwarded-CoRecipientsAward: “Establishing the Controlling Parameters of Ignition in High-Speed Flow”AIAA Citation: AIAA 2016-0658
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Edward A LukeAwarded-CoRecipientsAward: “Establishing the Controlling Parameters of Ignition in High-Speed Flow”AIAA Citation: AIAA 2016-0658
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Dr Timothy OmbrelloAir Force Research LaboratoryAwarded-CoRecipientsAward: “Establishing the Controlling Parameters of Ignition in High-Speed Flow”AIAA Citation: AIAA 2016-0658
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Dr David M PetersonAwarded-CoRecipientsAward: “Establishing the Controlling Parameters of Ignition in High-Speed Flow”AIAA Citation: AIAA 2016-0658
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Dr Kohei OzawaKyushu Institute of TechnologyAwarded-CoRecipientsAward: “Flight Performance Simulations of Vertical Launched Sounding Rockets Using Altering-Intensity Swirling-Oxidizer-Flow-Type Hybrid Motors”AIAA Citation: AIAA 2015-3832
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Prof Toru ShimadaJapan Aerospace Exploration AgencyAwarded-CoRecipientsAward: “Flight Performance Simulations of Vertical Launched Sounding Rockets Using Altering-Intensity Swirling-Oxidizer-Flow-Type Hybrid Motors”AIAA Citation: AIAA 2015-3832
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Dr Richard D BranamThe University of AlabamaAwarded-CoRecipientsAward: “Non-Invasive Hall Current Distribution Measurement in a Hall Effect Thruster”AIAA Citation: AIAA 2015-4005
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Dr Casey C FarnellColorado State UniversityAwarded-CoRecipientsAward: “Non-Invasive Hall Current Distribution Measurement in a Hall Effect Thruster”AIAA Citation: AIAA 2015-4005
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Mr. Cody C FarnellColorado State UniversityAwarded-CoRecipientsAward: “Non-Invasive Hall Current Distribution Measurement in a Hall Effect Thruster”AIAA Citation: AIAA 2015-4005
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Dr David LiuAir Force Institute of TechnologyAwarded-CoRecipientsAward: “Non-Invasive Hall Current Distribution Measurement in a Hall Effect Thruster”AIAA Citation: AIAA 2015-4005
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Mr. Rafael A MartinezAwarded-CoRecipientsAward: “Non-Invasive Hall Current Distribution Measurement in a Hall Effect Thruster”AIAA Citation: AIAA 2015-4005
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Carl R MullinsBusek Co. Inc.Awarded-CoRecipientsAward: “Non-Invasive Hall Current Distribution Measurement in a Hall Effect Thruster”AIAA Citation: AIAA 2015-4005
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Dr John D WilliamsColorado State UniversityAwarded-CoRecipientsAward: “Non-Invasive Hall Current Distribution Measurement in a Hall Effect Thruster”AIAA Citation: AIAA 2015-4005
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Dr Brian J CantwellStanford UniversityAwarded-CoRecipientsAward: “Visualization Study of Self-Pressurizing Propellant Tank Dynamics”AIAA Citation: AIAA 2015-3829
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Mr Greg ZilliacNASA-AmesAwarded-CoRecipientsAward: “Visualization Study of Self-Pressurizing Propellant Tank Dynamics”AIAA Citation: AIAA 2015-3829
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Mr Jonah E ZimmermanAwarded-CoRecipientsAward: “Visualization Study of Self-Pressurizing Propellant Tank Dynamics”AIAA Citation: AIAA 2015-3829
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Mr Sascha KaiserBauhaus Luftfahrt e. V.Awarded-CoRecipientsAward: A Composite Cycle Engine Concept with Hecto-Pressure RatioAIAA Citation: AIAA 2015-4028
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Dr Arne SeitzDLR-BraunschweigAwarded-CoRecipientsAward: A Composite Cycle Engine Concept with Hecto-Pressure RatioAIAA Citation: AIAA 2015-4028
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Dr Stanley K BorowskiAwarded-CoRecipientsAward: Affordable Development and Demonstration of a Small NTR Engine and Stage: A Preliminary NASA, DOE and Industry AssessmentAIAA Citation: AIAA 2015-3774
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Prof Claude Russell Joyner IIAerojet RocketdyneAwarded-CoRecipientsAward: Affordable Development and Demonstration of a Small NTR Engine and Stage: A Preliminary NASA, DOE and Industry AssessmentAIAA Citation: AIAA 2015-3774
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Mr David R McCurdyVantage Partners, LimitedAwarded-CoRecipientsAward: Affordable Development and Demonstration of a Small NTR Engine and Stage: A Preliminary NASA, DOE and Industry AssessmentAIAA Citation: AIAA 2015-3774
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Dr Arthur Louis QuallsOak Ridge National LaboratoryAwarded-CoRecipientsAward: Affordable Development and Demonstration of a Small NTR Engine and Stage: A Preliminary NASA, DOE and Industry AssessmentAIAA Citation: AIAA 2015-3774
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Mr. James E WernerIdaho National LaboratoryAwarded-CoRecipientsAward: Affordable Development and Demonstration of a Small NTR Engine and Stage: A Preliminary NASA, DOE and Industry AssessmentAIAA Citation: AIAA 2015=3774
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Ms Luisa A Cabrera MaynezAwarded-CoRecipientsAward: Component and System Modeling of a Direct Power Extraction SystemAIAA Citation: AIAA 2016-0990
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Dr Ahsan R ChoudhuriUniversity of Texas at El PasoAwarded-CoRecipientsAward: Component and System Modeling of a Direct Power Extraction SystemAIAA Citation: AIAA 2016-0990
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Mr Manuel J HernandezAwarded-CoRecipientsAward: Component and System Modeling of a Direct Power Extraction SystemAIAA Citation: AIAA 2016-0990
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Dr Norman D Love JrThe University of Texas El PasoAwarded-CoRecipientsAward: Component and System Modeling of a Direct Power Extraction SystemAIAA Citation: AIAA 2016-0990
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Andrew S FistAwarded-CoRecipientsAward: Improved Mean Flow Solution for Solid Rocket Motors with a Naturally Developing Swirling MotionAIAA Citation: AIAA 2014-4016
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Prof Joseph Majdalani PEAuburn UniversityAwarded-CoRecipientsAward: Improved Mean Flow Solution for Solid Rocket Motors with a Naturally Developing Swirling MotionAIAA Citation: AIAA 2014-4016
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Mr Terrence L Connell JrThe Pennsylvania State UniversityAwarded-CoRecipientsAward: Multi-Injector Impinging Jet Studies of Ignition Delay for Hydrogen Peroxide and Gelled Hydrocarbon Fuel Containing Reactive or Catalytic ParticlesAIAA Citation: AIAA 2015-3972
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Prof Benveniste NatanTechnion - Israel Institute of TechnologyAwarded-CoRecipientsAward: Multi-Injector Impinging Jet Studies of Ignition Delay for Hydrogen Peroxide and Gelled Hydrocarbon Fuel Containing Reactive or Catalytic ParticlesAIAA Citation: AIAA 2015-3972
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Prof Grant A RishaPennsylvania State University AltoonaAwarded-CoRecipientsAward: Multi-Injector Impinging Jet Studies of Ignition Delay for Hydrogen Peroxide and Gelled Hydrocarbon Fuel Containing Reactive or Catalytic ParticlesAIAA Citation: AIAA 2015-3972
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Dr Luciene D VillarInstitute of Aeronautics and SpaceAwarded-CoRecipientsAward: Time-Temperature Superposition Principle Applied to Thermally Aged Composite PropellantAIAA Citation: AIAA 2015-4107
2015
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Dr Thomas M BerensAIRBUS Defence and SpaceAwarded-CoRecipientsAward: “Numerical and Experimental Investigations on Highly Integrated Subsonic Air Intakes”AIAA Citation: AIAA 2014-0722
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Dr Nicola CeresolaAlenia AeronauticaAwarded-CoRecipientsAward: “Numerical and Experimental Investigations on Highly Integrated Subsonic Air Intakes”AIAA Citation: AIAA 2014-0722
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Mrs Anne-Laure DELOTONERAAwarded-CoRecipientsAward: “Numerical and Experimental Investigations on Highly Integrated Subsonic Air Intakes”AIAA Citation: AIAA 2014-0722
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Mr David E Funes-SebastianAIRBUS Defence and SpaceAwarded-CoRecipientsAward: “Numerical and Experimental Investigations on Highly Integrated Subsonic Air Intakes”AIAA Citation: AIAA 2014-0722
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Dr Martin ReinDLR - German Aerospace CenterAwarded-CoRecipientsAward: “Numerical and Experimental Investigations on Highly Integrated Subsonic Air Intakes”AIAA Citation: AIAA 2014-0722
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Eur Ing Luis P Ruiz-CalaveraAIRBUS Defence and SpaceAwarded-CoRecipientsAward: “Numerical and Experimental Investigations on Highly Integrated Subsonic Air Intakes”AIAA Citation: AIAA 2014-0722
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Mr. Michael SaterskogHjortronvagen 73Awarded-CoRecipientsAward: “Numerical and Experimental Investigations on Highly Integrated Subsonic Air Intakes”AIAA Citation: AIAA 2014-0722
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Mr Magnus H TormalmFOIAwarded-CoRecipientsAward: “Numerical and Experimental Investigations on Highly Integrated Subsonic Air Intakes”AIAA Citation: AIAA 2014-0722
2014
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Dr Stanley K BorowskiAwarded-CoRecipientsAward: A One-year Round Trip Crewed Mission to Mars using Bimodal Nuclear Thermal and Electric Propulsion (BNTEP)AIAA Citation: AIAA 2013-4076
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Mr David R McCurdyVantage Partners, LimitedAwarded-CoRecipientsAward: A One-year Round Trip Crewed Mission to Mars using Bimodal Nuclear Thermal and Electric Propulsion (BNTEP)AIAA Citation: AIAA 2013-4076
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Ms. Laura M BurkeNASA-Glenn Research CenterAwarded-CoRecipientsAward: A One-year Round Trip Crewed Mission to Mars using Bimodal Nuclear Thermal and Electric Propulsion (BNTEP),”AIAA Citation: AIAA 2013-4076
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Dr Hans-Detlev KuehlTU Dortmund UniversityAwarded-CoRecipientsAward: A Review of Models for Appendix Gap Losses in Stirling Cycle MachinesAIAA Citation: AIAA 2013-3613
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Mr Jens PfeifferLaboratory of ThermodynamicsAwarded-CoRecipientsAward: A Review of Models for Appendix Gap Losses in Stirling Cycle MachinesAIAA Citation: AIAA 2013-3613
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Dr Dan M GoebelJet Propulsion LaboratoryAwarded-CoRecipientsAward: Conducting Wall Hall ThrustersAIAA Citation: AIAA 2013-4117
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Dr Richard R HoferJet Propulsion LaboratoryAwarded-CoRecipientsAward: Conducting Wall Hall ThrustersAIAA Citation: AIAA 2013-4117
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Dr Ira KatzJet Propulsion LaboratoryAwarded-CoRecipientsAward: Conducting Wall Hall ThrustersAIAA Citation: AIAA 2013-4117
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Dr Ioannis G MikellidesJet Propulsion LaboratoryAwarded-CoRecipientsAward: Conducting Wall Hall ThrustersAIAA Citation: AIAA 2013-4117
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Dr James E PolkJet Propulsion LaboratoryAwarded-CoRecipientsAward: Conducting Wall Hall ThrustersAIAA Citation: AIAA 2013-4117
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Mr Nicolas BellomoAwarded-CoRecipientsAward: Development and Flight Testing of a Hybrid Rocket Booster for UAV Assisted Take OffAIAA Citation: AIAA 2013-4140
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Dr Alberto BettellaCISAS-University of PadovaAwarded-CoRecipientsAward: Development and Flight Testing of a Hybrid Rocket Booster for UAV Assisted Take OffAIAA Citation: AIAA 2013-4140
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Eur Ing Federico MorettoUniversita di PadovaAwarded-CoRecipientsAward: Development and Flight Testing of a Hybrid Rocket Booster for UAV Assisted Take OffAIAA Citation: AIAA 2013-4140
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Dr Daniele PavarinUniversità degli Studi di PadovaAwarded-CoRecipientsAward: Development and Flight Testing of a Hybrid Rocket Booster for UAV Assisted Take OffAIAA Citation: AIAA 2013-4140
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Michael McPhersonDigital Solid State PropulsionAwarded-CoRecipientsAward: Electric Solid Propellants: A Safe, Micro to Macro Propulsion TechnologyAIAA Citation: AIAA 2013-4168
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Dr Wayne N SawkaDSSP INCAwarded-CoRecipientsAward: Electric Solid Propellants: A Safe, Micro to Macro Propulsion TechnologyAIAA Citation: AIAA 2013-4168
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Dr Brian J CantwellStanford UniversityAwarded-CoRecipientsAward: Mass Flow Rate and Isolation Characteristics of Injectors for Use with Self-Pressurizing Oxidizers in Hybrid RocketsAIAA Citation: AIAA 2013-3636
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Dr Benjamin S WaxmanBlue Origin LLCAwarded-CoRecipientsAward: Mass Flow Rate and Isolation Characteristics of Injectors for Use with Self-Pressurizing Oxidizers in Hybrid RocketsAIAA Citation: AIAA 2013-3636
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Mr Greg ZilliacNASA-AmesAwarded-CoRecipientsAward: Mass Flow Rate and Isolation Characteristics of Injectors for Use with Self-Pressurizing Oxidizers in Hybrid RocketsAIAA Citation: AIAA 2013-3636
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Mr Jonah E ZimmermanAwarded-CoRecipientsAward: Mass Flow Rate and Isolation Characteristics of Injectors for Use with Self-Pressurizing Oxidizers in Hybrid RocketsAIAA Citation: AIAA 2013-3636
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Mrs Amy K ChicatelliAwarded-CoRecipientsAward: Model-Based Control of a Nonlinear Aircraft Engine Simulation using an Optimal Tuner Kalman Filter ApproachAIAA Citation: AIAA 2013-4002
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Joseph W ConnollyNASA Glenn Research CenterAwarded-CoRecipientsAward: Model-Based Control of a Nonlinear Aircraft Engine Simulation using an Optimal Tuner Kalman Filter ApproachAIAA Citation: AIAA 2013-4002
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Mr Jeffrey CsankNASA Glenn Research CenterAwarded-CoRecipientsAward: Model-Based Control of a Nonlinear Aircraft Engine Simulation using an Optimal Tuner Kalman Filter ApproachAIAA Citation: AIAA 2013-4002
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Prof Hyoung Jin KimKyung Hee UniversityAwarded-CoRecipientsAward: Optimal Inlet Shape Design of N2B Hybrid Wing Body ConfigurationAIAA Citation: AIAA 2012-3917
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Dr Philipp BehruziArianeGroupAwarded-CoRecipientsAward: Passive Phase Separation in Cryogenic Upper Stage TanksAIAA Citation: AIAA 2013-3905
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Salvatore M OritiNASA Glenn Research CenterAwardedAward: Performance Measurement of Advanced Stirling Convertors (ASC-E3)AIAA Citation: AIAA 2013-3813
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Mr Christoph Michael ArndtAwarded-CoRecipientsAward: Thermo-Acoustic Coupling in Swirl-Stabilized Flames with Helical VorticesAIAA Citation: AIAA 2013-3650
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Vincent Caux-BriseboisAwarded-CoRecipientsAward: Thermo-Acoustic Coupling in Swirl-Stabilized Flames with Helical VorticesAIAA Citation: AIAA 2013-3650
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Prof Adam M SteinbergGeorgia Institute of TechnologyAwarded-CoRecipientsAward: Thermo-Acoustic Coupling in Swirl-Stabilized Flames with Helical VorticesAIAA Citation: AIAA 2013-3650
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Dr Datta V GaitondeThe Ohio State UniversityAwarded-CoRecipientsAward: Unsteady Three-Dimensional Phenomena in Mode-Transition Simulations of the HIFiRE-2 Scramjet FlowpathAIAA Citation: AIAA 2013-3753
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Dr Robert John YentschAwarded-CoRecipientsAward: Unsteady Three-Dimensional Phenomena in Mode-Transition Simulations of the HIFiRE-2 Scramjet FlowpathAIAA Citation: AIAA 2013-3753
2013
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Prof Timothy S FisherUCLAAwarded-CoRecipientsAward: "Carbon Nanotube Arrays for Enhanced Thermal Interfaces to Thermoelectric Modules"AIAA Citation: AIAA 2012-4048
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Ms Kimberly SaviersAwarded-CoRecipientsAward: "Carbon Nanotube Arrays for Enhanced Thermal Interfaces to Thermoelectric Modules"AIAA Citation: AIAA 2012-4048
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Mr Pete F CrudgingtonCross Manufacturing Company (1938) LtdAwarded-CoRecipientsAward: , “A Novel High temperature non-Contact Dynamic Seal”AIAA Citation: AIAA 2012-4004
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Dr Dan M GoebelJet Propulsion LaboratoryAwarded-CoRecipientsAward: “Design of a Laboratory Hall Thruster with Magnetically Shielded Channel Walls, Phase III: Comparison of Theory with Experiment"AIAA Citation: AIAA 2012-3789
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Dr Richard R HoferJet Propulsion LaboratoryAwarded-CoRecipientsAward: “Design of a Laboratory Hall Thruster with Magnetically Shielded Channel Walls, Phase III: Comparison of Theory with Experiment"AIAA Citation: AIAA 2012-3789
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Dr Ira KatzJet Propulsion LaboratoryAwarded-CoRecipientsAward: “Design of a Laboratory Hall Thruster with Magnetically Shielded Channel Walls, Phase III: Comparison of Theory with Experiment"AIAA Citation: AIAA 2012-3789
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Dr Ioannis G MikellidesJet Propulsion LaboratoryAwarded-CoRecipientsAward: “Design of a Laboratory Hall Thruster with Magnetically Shielded Channel Walls, Phase III: Comparison of Theory with Experiment"AIAA Citation: AIAA 2012-3789
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Shannon D EilersAwarded-CoRecipientsAward: “Development and Testing of the Regeneratively Cooled Multiple Use Plug Hybrid (for) Nanosats (MUPHyN) Motor”AIAA Citation: AIAA 2013-4199
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Mr Zachary W PetersonAwarded-CoRecipientsAward: “Development and Testing of the Regeneratively Cooled Multiple Use Plug Hybrid (for) Nanosats (MUPHyN) Motor”AIAA Citation: AIAA 2013-4199
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Dr Stephen A WhitmoreUtah State UniversityAwarded-CoRecipientsAward: “Development and Testing of the Regeneratively Cooled Multiple Use Plug Hybrid (for) Nanosats (MUPHyN) Motor”AIAA Citation: AIAA 2013-4199
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Prof Christian O PaschereitTechnical University of BerlinAwarded-CoRecipientsAward: “Influence of Steam Dilution on NOx Formation in Premixed Natural Gas and Hydrogen Flames,”AIAA Citation: AIAA 2012-1272
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Miss Rebecca Lynn HayAdvanced Cooling Technologies, IncAwarded-CoRecipientsAward: “Long-Lived Venus Lander Thermal Management System Design”AIAA Citation: AIAA 2012-3892
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Mr. Andrew J SlippeyRochester Institute of TechnologyAwarded-CoRecipientsAward: “Long-Lived Venus Lander Thermal Management System Design”AIAA Citation: AIAA 2012-3892
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Dr Calin TarauAdvanced Cooling TechnologiesAwarded-CoRecipientsAward: “Long-Lived Venus Lander Thermal Management System Design”AIAA Citation: AIAA 2012-3892
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Dr Robert A BaurleNASA-Langley Research CenterAwarded-CoRecipientsAward: “Low-Dissipation Advection Schemes Designed for Large Eddy Simulations of Hypersonic Propulsion Systems"AIAA Citation: AIAA 2012-4263
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William S BlackAwarded-CoRecipientsAward: “Low-Dissipation Advection Schemes Designed for Large Eddy Simulations of Hypersonic Propulsion Systems"AIAA Citation: AIAA 2013-4263
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Dr Travis C FisherSandia National LaboratoriesAwarded-CoRecipientsAward: “Low-Dissipation Advection Schemes Designed for Large Eddy Simulations of Hypersonic Propulsion Systems"AIAA Citation: AIAA 2013-4263
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Dr Jesse QuinlanNASA Langley Research CenterAwarded-CoRecipientsAward: “Low-Dissipation Advection Schemes Designed for Large Eddy Simulations of Hypersonic Propulsion Systems"AIAA Citation: AIAA 203-4263
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Jeffery A WhiteNASA-Langley Research CenterAwarded-CoRecipientsAward: “Low-Dissipation Advection Schemes Designed for Large Eddy Simulations of Hypersonic Propulsion Systems"AIAA Citation: AIAA 2012-4263
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Dr Eric W DavisInstitute for Advanced Studies at AustinAwardedAward: Faster-Than-Light Space Warps, Status and Next StepsAIAA Citation: AIAA 2012-3860
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Jan DeekenDLR-German Aerospace CenterAwarded-CoRecipientsAward: Investigation of the API-Injection Concept in a LOX/LH2 Combustion Chamber at GG/PB Operation ConditionsAIAA Citation: AIAA 2012-3867
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Prof Oskar J HaidnTechnische Universität MünchenAwarded-CoRecipientsAward: Investigation of the API-Injection Concept in a LOX/LH2 Combustion Chamber at GG/PB Operation ConditionsAIAA Citation: AIAA 2012-3867
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Dr Dimitry SuslovDLR - German Aerospace CenterAwarded-CoRecipientsAward: Investigation of the API-Injection Concept in a LOX/LH2 Combustion Chamber at GG/PB Operation ConditionsAIAA Citation: AIAA 2012-3867
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Dr Meng-Sing LiouNASA Glenn Research CenterAwarded-CoRecipientsAward: Optimal Inlet Shape Design of N2B Hybrid Wing Body ConfigurationAIAA Citation: AIAA 2013-3917
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Dr P. J. BowenCardiff UniversityAwarded-CoRecipientsAward: Tangential Velocity Effects and Correlations for Blow-Off and Flashback in a Generic Swirl Burner and the Effect of a Hydrogen containing FuelAIAA Citation: AIAA 2013-0736
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Prof Nicholas SyredCardiff UniversityAwarded-CoRecipientsAward: Tangential Velocity Effects and Correlations for Blow-Off and Flashback in a Generic Swirl Burner and the Effect of a Hydrogen containing FuelAIAA Citation: AIAA 2013-0736
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Mr Germain BoyerAwarded-CoRecipientsAward: Theoretical Investigation of Parietal Vortex Shedding in Solid Rocket MotorsAIAA Citation: AIAA 2012-3825
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Prof Gregoire CasalisONERAAwarded-CoRecipientsAward: Theoretical Investigation of Parietal Vortex Shedding in Solid Rocket MotorsAIAA Citation: AIAA 2012-3825
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Dr Jean-luc EstivalezesONERAAwarded-CoRecipientsAward: Theoretical Investigation of Parietal Vortex Shedding in Solid Rocket MotorsAIAA Citation: AIAA 2012-3825
2012
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Eur Ing Francesco BaratoCISAS-University of PadovaAwarded-CoRecipientsAward: “A Numerical Model to Analyze the Transient Behavior and Instabilities on Hybrid Rocket Motors”AIAA Citation: AIAA 2011-5538
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Mr Nicolas BellomoAwarded-CoRecipientsAward: “A Numerical Model to Analyze the Transient Behavior and Instabilities on Hybrid Rocket Motors”AIAA Citation: AIAA 2011-5538
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Dr Alberto BettellaCISAS-University of PadovaAwarded-CoRecipientsAward: “A Numerical Model to Analyze the Transient Behavior and Instabilities on Hybrid Rocket Motors”AIAA Citation: AIAA 2011-5538
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Dr Martina FaenzaNammo Raufoss ASAwarded-CoRecipientsAward: “A Numerical Model to Analyze the Transient Behavior and Instabilities on Hybrid Rocket Motors”AIAA Citation: AIAA 2011-5538
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Eur Ing Marta LazzarinCISAS-University of PadovaAwarded-CoRecipientsAward: “A Numerical Model to Analyze the Transient Behavior and Instabilities on Hybrid Rocket Motors”AIAA Citation: AIAA 2011-5538
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Dr Daniele PavarinUniversità degli Studi di PadovaAwarded-CoRecipientsAward: “A Numerical Model to Analyze the Transient Behavior and Instabilities on Hybrid Rocket Motors”AIAA Citation: AIAA 2011-5538
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Dan BaruzziniLockheed Martin AeronauticsAwarded-CoRecipientsAward: “Addressing Corner Interactions Generated by Oblique Shock-Waves In Unswept Right-Angle Corners and Implications for High-Speed Inlets”AIAA Citation: AIAA 2012-0275
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Daniel N MillerLockheed Martin AeronauticsAwarded-CoRecipientsAward: “Addressing Corner Interactions Generated by Oblique Shock-Waves In Unswept Right-Angle Corners and Implications for High-Speed Inlets”AIAA Citation: AIAA 2012-0275
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Dr Luigi De LucaPolitecnico Di MilanoAwarded-CoRecipientsAward: “Ballistic and Rheological Characterization of Paraffin-Based Fuels for Hybrid Rocket Propulsion”AIAA Citation: AIAA 2011-5680
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Dr Luciano GalfettiPolitecnico di MilanoAwarded-CoRecipientsAward: “Ballistic and Rheological Characterization of Paraffin-Based Fuels for Hybrid Rocket Propulsion”AIAA Citation: AIAA 2011-5680
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Dr Filippo MaggiPolitecnico Di MilanoAwarded-CoRecipientsAward: “Ballistic and Rheological Characterization of Paraffin-Based Fuels for Hybrid Rocket Propulsion”AIAA Citation: AIAA 2011-5680
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A. Scott HoweJet Propulsion LaboratoryAwarded-CoRecipientsAward: “Habitat Water Wall for Water, Solids, and Atmosphere Recycle and Reuse”AIAA Citation: AIAA 2011-5018
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Dr Yoshifumi InataniJapan Aerospace Exploration AgencyAwarded-CoRecipientsAward: “Heat Exchange and Pressure Drop Enhanced by Sloshing”AIAA Citation: AIAA 2011-5682
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Prof Chihiro InoueUniversity of TokyoAwarded-CoRecipientsAward: “Heat Exchange and Pressure Drop Enhanced by Sloshing”AIAA Citation: AIAA 2011-5682
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Kazutoshi IshikawaNational Aerospace LaboratoriesAwarded-CoRecipientsAward: “Heat Exchange and Pressure Drop Enhanced by Sloshing”AIAA Citation: AIAA 2011-5682
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Dr Kiyoshi KinefuchiJapan Aerospace Exploration AgencyAwarded-CoRecipientsAward: “Heat Exchange and Pressure Drop Enhanced by Sloshing”AIAA Citation: AIAA 2011-5682
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Yoshihiro NaruoJapan Aerospace Exploration AgencyAwarded-CoRecipientsAward: “Heat Exchange and Pressure Drop Enhanced by Sloshing”AIAA Citation: AIAA 2011-5682
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Dr Satoshi NonakaJapan Aerospace Exploration AgencyAwarded-CoRecipientsAward: “Heat Exchange and Pressure Drop Enhanced by Sloshing”AIAA Citation: AIAA 2011-5682
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Dr Kohei OkitaThe University of TokyoAwarded-CoRecipientsAward: “Heat Exchange and Pressure Drop Enhanced by Sloshing”AIAA Citation: AIAA 2011-5682
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Mr Daizo SugimoriJapan Aerospace Exploration AgencyAwarded-CoRecipientsAward: “Heat Exchange and Pressure Drop Enhanced by Sloshing”AIAA Citation: AIAA 2011-5682
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Prof Toshinori WatanabeThe University of TokyoAwarded-CoRecipientsAward: “Heat Exchange and Pressure Drop Enhanced by Sloshing”AIAA Citation: AIAA 2011-5682
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Dr Mirko GambaUniversity of MichiganAwarded-CoRecipientsAward: “Ignition and Near-Wall Burning in Transverse Hydrogen Jets in Supersonic Crossflow”AIAA Citation: AIAA 2011-3539
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Prof Ronald K HansonStanford UniversityAwarded-CoRecipientsAward: “Ignition and Near-Wall Burning in Transverse Hydrogen Jets in Supersonic Crossflow”AIAA Citation: AIAA 2011-0319
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Prof M. MungalStanford UniversityAwarded-CoRecipientsAward: “Ignition and Near-Wall Burning in Transverse Hydrogen Jets in Supersonic Crossflow”AIAA Citation: AIAA 2011-0319
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Dr Stanley K BorowskiAwarded-CoRecipientsAward: “Lower Thrust Engine Options Based on the Small Nuclear Rocket Engine Design”AIAA Citation: AIAA 2011-5846
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Mr James E FittjeVantage PartnersAwarded-CoRecipientsAward: “Lower Thrust Engine Options Based on the Small Nuclear Rocket Engine Design”AIAA Citation: AIAA 2011-5846
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Bruce G SchnitzlerOak Ridge National LabAwarded-CoRecipientsAward: “Lower Thrust Engine Options Based on the Small Nuclear Rocket Engine Design”AIAA Citation: AIAA 2011-5846
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Prof Ashwani K GuptaUniversity of MarylandAwarded-CoRecipientsAward: “Mixture Preparation Effects On Distributed Combustion For Gas Turbine Applications”AIAA Citation: AIAA 2012-0930
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Dr Campbell D CarterU.S. Air Force Research LaboratoryAwarded-CoRecipientsAward: “Particle Image Velocimetry in an Isothermal and Exothermic High-Speed Cavity”AIAA Citation: AIAA 2012-0330
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Dr KuangYu HsuInnovative Scientific Solutions IncorporatedAwarded-CoRecipientsAward: “Particle Image Velocimetry in an Isothermal and Exothermic High-Speed Cavity”AIAA Citation: AIAA 2012-0330
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Dr Steven G TuttleNaval Research Laboratory - Combustion Dynamics and Modeling SectionAwarded-CoRecipientsAward: “Particle Image Velocimetry in an Isothermal and Exothermic High-Speed Cavity”AIAA Citation: AIAA 2012-0330
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Dr Neal D DomelLockheed Martin AeronauticsAwarded-CoRecipientsAward: Addressing Corner Interactions Generated by Oblique Shock-Waves In Unswept Right-Angle Corners and Implications for High-Speed InletsAIAA Citation: IAA 2012-0275
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Ioana Diana BroomeAwarded-CoRecipientsAward: Design and Analysis of a Multi-Window Aperture Structure for a Small Particle Solar ReceiverAIAA Citation: AIAA 2011-5900
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Prof Fletcher J. MillerSan Diego State UniversityAwarded-CoRecipientsAward: Design and Analysis of a Multi-Window Aperture Structure for a Small Particle Solar ReceiverAIAA Citation: AIAA 2011-5900
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Prof Takehiro HimenoUniversity of TokyoAwarded-CoRecipientsAward: Heat Exchange and Pressure Drop Enhanced by SloshingAIAA Citation: AIAA 2011-5682
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Dr Yutaka UmemuraJAXAAwarded-CoRecipientsAward: Heat Exchange and Pressure Drop Enhanced by SloshingAIAA Citation: AIAA 2011-5682
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Mr. John R BrophyJet Propulsion LaboratoryAwarded-CoRecipientsAward: In-Flight Operation of the Dawn Ion Propulsion System Through Orbit Capture at VestaAIAA Citation: AIAA 2011-5661
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Charles E GarnerJet Propulsion LaboratoryAwarded-CoRecipientsAward: In-Flight Operation of the Dawn Ion Propulsion System Through Orbit Capture at VestaAIAA Citation: AIAA 2011-5661
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Mr. Steven MikesJet Propulsion LaboratoryAwarded-CoRecipientsAward: In-Flight Operation of the Dawn Ion Propulsion System Through Orbit Capture at VestaAIAA Citation: AIAA 2011-5661
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Dr Marc D RaymanJet Propulsion LaboratoryAwarded-CoRecipientsAward: In-Flight Operation of the Dawn Ion Propulsion System Through Orbit Capture at VestaAIAA Citation: AIAA 2011-5661
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Maxwell H BriggsAwarded-CoRecipientsAward: Overview of Heat Addition and Efficiency Predictions for an Advanced Stirling ConvertorAIAA Citation: AIAA 2011-5576
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Dr Terry V ReidNASA Glenn Research CenterAwarded-CoRecipientsAward: Overview of Heat Addition and Efficiency Predictions for an Advanced Stirling ConvertorAIAA Citation: AIAA 2011-5576
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Nicholas A SchiferNASAAwarded-CoRecipientsAward: Overview of Heat Addition and Efficiency Predictions for an Advanced Stirling ConvertorAIAA Citation: AIAA 2011-5576
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Scott D WilsonNASA Glenn Research CenterAwarded-CoRecipientsAward: Overview of Heat Addition and Efficiency Predictions for an Advanced Stirling ConvertorAIAA Citation: AIAA 2011-5576
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Mr Nathan GibsonGE AviationAwarded-CoRecipientsAward: Second Generation Air-to-Air Mechanical Seal Design and PerformanceAIAA Citation: AIAA 2011-5636
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Dr Malak F MalakAllied Signal Aerospace CoAwarded-CoRecipientsAward: Second Generation Air-to-Air Mechanical Seal Design and PerformanceAIAA Citation: AIAA 2011-5636
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Dr Mark SalitaAwardedAward: Unanticipated Problems and Misunderstood Phenomena in and Around Solid RocketsAIAA Citation: AIAA 2011-5956
2011
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Dr Frederick G HarmonAFITAwarded-CoRecipientsAward: Conceptual Design Tool for Micro Air Vehicles with Hybrid Power SystemsAIAA Citation: AIAA 2010-6688
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CPT Paul M HradAwarded-CoRecipientsAward: Conceptual Design Tool for Micro Air Vehicles with Hybrid Power SystemsAIAA Citation: AIAA 2010-6688
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Mr John T LopezAwarded-CoRecipientsAward: Quantifying the Effects of Long Term Storage on Extended Cycling for Lithium-Ion BatteriesAIAA Citation: AIAA 2010-6924
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Mr. Chris D PearsonAwarded-CoRecipientsAward: Quantifying the Effects of Long Term Storage on Extended Cycling for Lithium-Ion BatteriesAIAA Citation: AIAA 2010-6924
2010
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Dr James E PolkJet Propulsion LaboratoryAwardedAward: Barium Depletion in Hollow Cathode EmittersAIAA Citation: AIAA 2009-5197
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Mr. Eric BoydPennsylvania State UniversityAwarded-CoRecipientsAward: Comparison of Nozzle Throat Erosion Behavior in a Solid Propellant Rocket Motor and a SimulatorAIAA Citation: AIAA 2009-5421
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Dr Andrew CortopassiThe Aerospace CorporationAwarded-CoRecipientsAward: Comparison of Nozzle Throat Erosion Behavior in a Solid Propellant Rocket Motor and a SimulatorAIAA Citation: AIAA 2009-5421
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Brian J EvansSpace Propulsion Group, Inc.Awarded-CoRecipientsAward: Comparison of Nozzle Throat Erosion Behavior in a Solid Propellant Rocket Motor and a SimulatorAIAA Citation: AIAA 2009-5421
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Bradley C AppelTexas A&M UnivAwarded-CoRecipientsAward: Development and Launch of the Purdue Hybrid Rocket Technology DemonstratorAIAA Citation: AIAA 2009-4842
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Dr Stephen D HeisterPurdue UniversityAwarded-CoRecipientsAward: Development and Launch of the Purdue Hybrid Rocket Technology DemonstratorAIAA Citation: AIAA 2009-4842
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Andrew K RettenmaierPurdue UniversityAwarded-CoRecipientsAward: Development and Launch of the Purdue Hybrid Rocket Technology DemonstratorAIAA Citation: AIAA 2009-4842
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Mr. John TsohasPurdue UniversityAwarded-CoRecipientsAward: Development and Launch of the Purdue Hybrid Rocket Technology DemonstratorAIAA Citation: AIAA 2009-4842
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Dr Matthias GrosseENERGETIXAwardedAward: Effect of a Diaphragm on Performance and Fuel Regression of a Laboratory Scale Hybrid Rocket Motor Using Nitrous Oxide and ParaffinAIAA Citation: AIAA 2009-5113
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Jordan T FarinaVirginia Polytechnic InstituteAwarded-CoRecipientsAward: Instrumentation, Modeling and Testing of a Gas Turbine Engine Using Lean Premixed Hydrogen CombustionAIAA Citation: AIAA 2009-5048
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Steve LeperaVA TechAwarded-CoRecipientsAward: Instrumentation, Modeling and Testing of a Gas Turbine Engine Using Lean Premixed Hydrogen CombustionAIAA Citation: AIAA 2009-5048
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Prof Walter F O'BrienVirginia TechAwarded-CoRecipientsAward: Instrumentation, Modeling and Testing of a Gas Turbine Engine Using Lean Premixed Hydrogen CombustionAIAA Citation: AIAA 2009-5048
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Matthew V PerryElectric Jet LLCAwarded-CoRecipientsAward: Instrumentation, Modeling and Testing of a Gas Turbine Engine Using Lean Premixed Hydrogen CombustionAIAA Citation: AIAA 2009-5048
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Dr Uri VandsburgerVPI/SUAwarded-CoRecipientsAward: Instrumentation, Modeling and Testing of a Gas Turbine Engine Using Lean Premixed Hydrogen CombustionAIAA Citation: AIAA 2009-5048
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Mr Adam ButtNASAAwarded-CoRecipientsAward: NASA Ares I Launch Vehicle Roll and Reaction Control Systems Design StatusAIAA Citation: AIAA 2009-5130
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Mr Hank M PittsThe Boeing CompanyAwarded-CoRecipientsAward: NASA Ares I Launch Vehicle Roll and Reaction Control Systems Design StatusAIAA Citation: AIAA 2009-5130
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Chris PoppNASA-Marshall Space Flight CenterAwarded-CoRecipientsAward: NASA Ares I Launch Vehicle Roll and Reaction Control Systems Design StatusAIAA Citation: AIAA 2009-5130
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Mr. David J SharpAllied Aerospace Industries IncAwarded-CoRecipientsAward: NASA Ares I Launch Vehicle Roll and Reaction Control Systems Design StatusAIAA Citation: AIAA 2009-5130
2007
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Yoshihiro ArakawaAwarded-CoRecipientsAward: Power Transmission to a Micro Aerial VehicleAIAA Citation: AIAA 2007-1003
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Mr. Shuhei KomatsuUniversity of TokyoAwarded-CoRecipientsAward: Power Transmission to a Micro Aerial VehicleAIAA Citation: AIAA 2007-1003
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Prof Kimiya KomurasakiThe University of TokyoAwarded-CoRecipientsAward: Power Transmission to a Micro Aerial VehicleAIAA Citation: AIAA 2007-1003
2005
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Dr Omar AbdelazizAwarded-CoRecipientsAward: Air Flow Regimes and Thermal Patterns in Climatized Tombs in Valley of KingsAIAA Citation: AIAA 2005-1444
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Prof Essam E KhalilCairo UniversityAwarded-CoRecipientsAward: Air Flow Regimes and Thermal Patterns in Climatized Tombs in Valley of KingsAIAA Citation: AIAA 2005-1444
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Mr. John CrittendenTriad Research Corporation Inc.Awarded-CoRecipientsAward: Demonstration of a Novel Combined Cooling and Power Gas Turbine with Water HarvestingAIAA Citation: AIAA 2005-0571
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Dr Jameel KhanUniversity of FloridaAwarded-CoRecipientsAward: Demonstration of a Novel Combined Cooling and Power Gas Turbine with Water HarvestingAIAA Citation: AIAA 2005-0571
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Dr William E LearUniversity of FloridaAwarded-CoRecipientsAward: Demonstration of a Novel Combined Cooling and Power Gas Turbine with Water HarvestingAIAA Citation: AIAA 2005-0571
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Prof S.A. SherifUniversity of FloridaAwarded-CoRecipientsAward: Demonstration of a Novel Combined Cooling and Power Gas Turbine with Water HarvestingAIAA Citation: AIAA 2005-0571
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Mr. Robert M ButtonNASA Glenn Research CenterAwarded-CoRecipientsAward: Distributed, Master-less Control of Modular DC-DC ConvertersAIAA Citation: AIAA 2004-5733
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Zhiqiang GaoCleveland State UniversityAwarded-CoRecipientsAward: Distributed, Master-less Control of Modular DC-DC ConvertersAIAA Citation: AIAA 2004-5733
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Michael S GrayCleveland State UniversityAwarded-CoRecipientsAward: Distributed, Master-less Control of Modular DC-DC ConvertersAIAA Citation: AIAA 2004-5733
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Mr. Edward J BrownLockheed Martin CorporationAwarded-CoRecipientsAward: Thermophotovoltaic Spectral ControlAIAA Citation: AIAA 2004-5762
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David DepoyLockheed Martin CorporationAwarded-CoRecipientsAward: Thermophotovoltaic Spectral ControlAIAA Citation: AIAA 2004-5762
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Mr. Edward GratrixRugate Technologies IncAwarded-CoRecipientsAward: Thermophotovoltaic Spectral ControlAIAA Citation: AIAA 2004-5762
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Mr. Thomas D Rahmlow Jr.Rugate Technologies IncAwarded-CoRecipientsAward: Thermophotovoltaic Spectral ControlAIAA Citation: AIAA 2004-5762
2004
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Jorge CamachoUniversity of Texas at El PasoAwarded-CoRecipientsAward: Characteristics of Nonbuoyant Elliptical Jet Diffusion FlamesAIAA Citation: AIAA 2004-0814
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Dr Ahsan R ChoudhuriUniversity of Texas at El PasoAwarded-CoRecipientsAward: Characteristics of Nonbuoyant Elliptical Jet Diffusion FlamesAIAA Citation: AIAA 2004-0824
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Dr Jonathan L FlemingTechsburgAwarded-CoRecipientsAward: Thermoelectric Power Generation for UAV ApplicationsAIAA Citation: AIAA 2003-6092
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Dr WingFai NgTechsburg, Inc.Awarded-CoRecipientsAward: Thermoelectric Power Generation for UAV ApplicationsAIAA Citation: AIAA 2003-6092