Aerodynamics Award Open for Nominations 10 November 2024 – 15 January 2025
The Aerodynamics Award, approved by the Board of Directors in 1983, is presented for meritorious achievement in the field of applied aerodynamics, recognizing notable contributions in the development, application, and evaluation of aerodynamic concepts and methods.
This annual award is generally presented at the AIAA AVIATION Forum/ASCEND.
Deadlines:
Accepting Online Nominations: 10 November
Nomination Deadline: 15 January
Endorsement Letters Deadline: 1 February
Award Recipients
2023
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Roy J Hartfield JrAuburn UniversityAwardedAward: 2023 AIAA Aerodynamics AwardAIAA Citation: For the development of fast and practical predictive approaches to the problem of aerodynamic analysis of air vehicles at both conceptual and preliminary design stages.
2022
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Prof Marilyn J SmithGeorgia Institute of TechnologyAwardedAward: 2022 AIAA Aerodynamics AwardAIAA Citation: “For contributions to the computational and theoretical aerodynamic analysis of static and dynamic systems with separated flows, particularly for vertical takeoff and landing rotorcraft vehicles.”
2021
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Dr Scott A MortonDoD HPCMPAwardedAward: 2021 AIAA Aerodynamics AwardAIAA Citation: For a career devoted to extending the application of CFD to challenging unsteady aerodynamic phenomena, such as transonic flutter, complex vortical flowfields, and maneuvering flight.
2020
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Dr Mark D MaughmerThe Pennsylvania State UniversityAwardedAward: 2020 Aerodynamics AwardAIAA Citation: For foundational developments in airfoil and wing design, advancement of novel airfoil configurations, and contributions to rotorcraft aeromechanics.
2019
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Mr Robert D Gregg IIIThe Boeing CompanyAwardedAward: 2019 Aerodynamics AwardAIAA Citation: “In recognition of innovations in Aircraft Design through inspirational leadership and technical contributions in the field of Aerodynamic design and advanced concepts.”
2018
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Prof Kenneth C HallDuke UniversityAwardedAward: 2018 Aerodynamics AwardAIAA Citation: For seminal contributions in the development of novel unsteady aerodynamic theories and analysis methods for internal and external flows.
2017
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Dr John A BenekAir Force Research Lab AFRL/RQAwardedAIAA Citation: For distinguished contributions to the development of the Chimera scheme making simulations over complex aerodynamic configurations feasible and for advancements in integrated CFD/experimental studies.
2016
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Dr Pieter G BuningNASA-Langley Research CenterAwardedAIAA Citation: In recognition of exceptional leadership, innovation and expertise in the field of overset grid CFD methods and applications that are used internationally for wide-spread advancements in the aerodynamic design and development of air and space vehicles.
2015
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Prof Russell M CummingsUS Air Force AcademyAwardedAward: -AIAA Citation: For a career devoted to predicting and understanding the vortical flowfields about aircraft at high angles of attack and during maneuvers
2014
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Dr Michael S SeligUniversity of Illinois at Urbana-ChampaignAwardedAIAA Citation: In recognition of outstanding contributions to applied aerodynamics research, design, and education, including leadership in the development and public dissemination of airfoil and propeller data.
2013
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Dr Neal T FrinkNASA-Langley Research CenterAwardedAIAA Citation: For meritorious achievement in the field of applied aerodynamics through notable contributions in the development, application, and evaluation of aerodynamic concepts and methods
2012
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Dr John C VassbergThe Boeing CompanyAwardedAIAA Citation: In recognition of outstanding achievements in the field of air vehicle aerodynamic design and optimization; and for exceptional leadership and technical expertise in advancing CFD drag reduction and prediction capabilities.
2011
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Preston A HenneAwardedAIAA Citation: In recognition of outstanding leadership and contribution in the aerodynamic field of low boom supersonics research.
2010
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Dr Thomas C CorkeUniversity of Notre DameAwardedAIAA Citation: For his strong commitment to academic and research achievement, consistent record of superior technical accomplishment, and numerous experimental and computational contributions to aerodynamics.
2009
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Dr Jubaraj SahuUS Army Research LaboratoryAwardedAIAA Citation: In recognition of outstanding contributions in development and application of unsteady aerodynamics of micro-adaptive flow control and demonstration of control authority of spinning munitions.
2008
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Prof Ramesh K AgarwalWashington University in St LouisAwardedAIAA Citation: For pioneering development of computational fluid dynamics methods and codes for the aerodynamic analysis and design of all categories of aerospace vehicles.
2007
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Dr Michael B BraggUniversity of WashingtonAwardedAIAA Citation: For pioneering research on the aerodynamic effects of ice accretion on aircraft and the aerodynamic phenomena responsible.
2006
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Mr William B BlakeAir Force Reseach LaboratoryAwardedAIAA Citation: For exceptional contributions to applied aerodynamic predictions through experimentation and empirical and engineering modeling.
2005
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Dr Robert M HallNASA-Langley Research CenterAwardedAIAA Citation: For outstanding contributions toward understanding the flow physics and configuration aerodynamics of high performance aircraft.
2004
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Jean M DeleryONERAAwardedAIAA Citation: For outstanding experimental contributions to the understanding of the flow physics of base flows, multi-flux nozzles, shock wave/boundary layer interaction and vortex breakdown
2003
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Dr Thomas J MuellerUniversity of Notre DameAwardedAIAA Citation: “For outstanding experimental contributions to the understanding of the flow physics of Low Reynolds number airfoils and wings.”
2002
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Mr Richard L CampbellNASA-Langley Research CenterAwardedAIAA Citation: For outstanding technical contributions toward advancement of rapid, high-fidelity aerodynamic design capability for complex aerospace configurations
2001
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Mr. Gerald L WinchenbachAwardedAIAA Citation: For outstanding achievement and significant contributions in experimental applied aerodynamic research within a free-flight ballistics range
2000
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C Edward LanAwardedAIAA Citation: For three decades of continuous contribution to the field of applied aerodynamics leading to the development of VORSTAB code, high-awind tunnel correction and unsteady aerodynamics
1999
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Mr. Frank T LynchAwardedAIAA Citation: For outstanding achievement in applied aerodynamics connected with the design of the DC-8, DC-9 and DC-10 airplanes and for technology leadership in the fields of propulsion/airframe integration, laminar flow control, viscous scaling and transonic wing and high-lift aerodynamics
1998
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M. L SpearmanAwardedAIAA Citation: For pioneering research and exceptional contributions in the field of supersonic aerodynamics which has impacted the design of essentially every supersonic aircraft and missile developed in the US since the1950''s
1997
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Werner K DahmNASA MSFCAwardedAIAA Citation: For meritorious performance and exceptional contributions in the aerodynamic design and analysis of strategic rockets and manned/unmanned launch vehicles
1996
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Mr. Jan R TuliniusRockwell International CorpAwardedAIAA Citation: For successful flight demonstration of a significant amount of supersonic laminar flow on a highly swept wing aircraft
1995
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Mr. Lawrence E PutnamAwardedAIAA Citation: For leadership in the advancement of applied computational fluid dynamic methods and the development and application of high Reynolds-number wind tunnel testing
1994
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Heinz A GerhardtAwardedAIAA Citation: For meritorious performance in all areas of aerodynamics as applied to high performance tactical aircraft
1993
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Dr Tuncer CebeciAwardedAIAA Citation: For sustained contributions to the understanding and numerical computation of viscous flows, especially the important problem of the transition in three-dimensional flows, and successfully applying basic research techniques to real aircraft problems.
1992
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Mr. Joe F ThompsonGeneral DynamicsAwardedAIAA Citation: For meritorious achievement in the field of applied aerodynamics recognizing notable contributions in numerical grid generation which have revolutionized computational aerodynamics for realistic configurations and complex flows
1991
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Dr Norman D MalmuthTeledyne Scientific CompanyAwardedAIAA Citation: For meritorious achievement in the field of applied aerodynamics and recognition for notable contributions in the development and application of combined asymptotics and numerics in the solution of transonic and hypersonic problems
1990
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Mr. Hans W GrellmannNorthrop Grumman CorporationAwardedAIAA Citation: In recognition of exceptional contributions in leading the B-2 aerodynamics team in their development of a highly efficient aircraft with outstanding handling properties despite the severe constraints imposed by low observability requirements
1989
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Edward N TinocoAwardedAIAA Citation: For meritorious achievement in the field of applied aerodynamics recognizing notable contributions in the development, application and evaluation of aerodynamics concepts and methods, and for the pursuit of pioneering applications of Advanced Computational Fluid Dynamics to commercial and military air vehicles analysis and design
1987
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Dr Robert H LiebeckThe Boeing CompanyAwardedAIAA Citation: For the development of the highly successful and widely used "Liebeck Airfoils" which have demonstrated lift-to-drag ratios as high as 235
1986
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Dr Bruce J HolmesSmartSky Networks, LLCAwardedAIAA Citation: For research excellence demonstrating the practicality of using natural laminar boundary layer flow to reduce the drag on modern, smooth aircraft surfaces
1985
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Dr Forrester T JohnsonAwardedAward: -AIAA Citation: For development of advanced aerodynamic panel methods used throughout the industry for commercial and military aircraft
1984
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Dr Lars E EricssonAwardedAIAA Citation: For outstanding aerodynamic advancements in the field of unsteady, separated and vortex flows, through experimental and analytical development and their application to the development of launch vehicles, space shuttle, re-entry vehicles, aircraft and missile configurations
1983
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Dr John E LamarAwardedAIAA Citation: For developing aerodynamic analysis and design methods for wings having strong leading-edge-vortex flow and for developing and experimentally verifying favorable shaping of wings and strakes to exploit vortex flow for performance improvement