Antony Jameson

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Luigi MartinelliPrinceton UniversityVerified email at princeton.edu
Peter VincentProfessor of Computational Fluid Dynamics, Department of Aeronautics, Imperial College LondonVerified email at imperial.ac.uk
Patrice CastonguayEngineering Specialist, Bombardier AerospaceVerified email at aero.bombardier.com
Freddie WitherdenAssistant Professor at Texas A&M UniversityVerified email at tamu.edu
Siva NadarajahMcGill UniversityVerified email at mcgill.ca
Chunlei Charles LiangProfessor of Mechanical and Aerospace Engineering, Clarkson UniversityVerified email at clarkson.edu
Kui OuHonda Aircraft CompanyVerified email at alumni.stanford.edu
David Michael WilliamsAssociate Professor in Mechanical Engineering, Pennsylvania State UniversityVerified email at psu.edu
Eli TurkelProfessor of Mathematics, Tel Aviv UniversityVerified email at post.tau.ac.il
Jonathan BullAlfa LavalVerified email at alfalaval.com
Dimitri MavriplisProfessor, Mechanical Engineering, University of WyomingVerified email at uwyo.edu
Z.J. WangUniversity of KansasVerified email at ku.edu
Kun XuChair Professor, Mathematics Department, Hong Kong University of Science and TechnologyVerified email at ust.hk
Joshua RomeroNVIDIA CorporationVerified email at nvidia.com
Feng LiuUniversity of California, IrvineVerified email at uci.edu
Manuel R. López MoralesStanford UniversityVerified email at stanford.edu
Abhishek SheshadriStanford UniversityVerified email at stanford.edu
Kartikey AsthanaPhD, Stanford UniversityVerified email at stanford.edu
Niles A. PierceMacArthur Professor, California Institute of TechnologyVerified email at caltech.edu
David Manosalvas-KjonoCo-founder & CEO of Aeromutable Corp. || ORISE Argonne Chain Reaction Innovations FellowVerified email at stanford.edu

Antony Jameson

Professor of Aerospace Engineering, Texas A&M University

Verified email at tamu.edu - Homepage

Computational Mechanics Aerodynamics Design


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Numerical solutions of the Euler equations by finite volume methods using Runge-Kutta time-stepping schemes A Jameson, W Schmidt, E Turkel AIAA 14th Fluid and Plasma Dynamic Conference 81 (1259), 1981	6048	1981
Aerodynamic design via control theory A Jameson Journal of scientific computing 3, 233-260, 1988	2302	1988
Time dependent calculations using multigrid, with applications to unsteady flows past airfoils and wings A Jameson 10th Computational fluid dynamics conference, 1596, 1991	2277	1991
Lower-upper symmetric-Gauss-Seidel method for the Euler and Navier-Stokes equations S Yoon, A Jameson AIAA journal 26 (9), 1025-1026, 1988	1663	1988
Optimum aerodynamic design using the Navier–Stokes equations A Jameson, L Martinelli, NA Pierce Theoretical and computational fluid dynamics 10 (1), 213-237, 1998	960	1998
Solution of the Euler equations for two dimensional transonic flow by a multigrid method A Jameson Applied mathematics and computation 13 (3-4), 327-355, 1983	692	1983
Lower-upper implicit schemes with multiple grids for the Euler equations A Jameson, S Yoon AIAA journal 25 (7), 929-935, 1987	677	1987
Optimum aerodynamic design using CFD and control theory A Jameson 12th computational fluid dynamics conference, 1729, 1995	584	1995
Calculation of inviscid transonic flow over a complete aircraft A Jameson, T Baker, N Weatherill 24th Aerospace Sciences Meeting, 1986	529	1986
Solution of the Euler equations for complex configurations A Jameson, T Baker 6th computational fluid dynamics conference danvers, 1929, 1983	522	1983
Analysis and design of numerical schemes for gas dynamics, 1: artificial diffusion, upwind biasing, limiters and their effect on accuracy and multigrid convergence A Jameson International Journal of Computational Fluid Dynamics 4 (3-4), 171-218, 1995	495	1995
Finite volume solution of the two-dimensional Euler equations on a regular triangular mesh A Jameson, D Mavriplis AIAA journal 24 (4), 611-618, 1986	471	1986
Constrained multipoint aerodynamic shape optimization using an adjoint formulation and parallel computers, part 2 JJ Reuther, A Jameson, JJ Alonso, MJ Rimllnger, D Saunders Journal of aircraft 36 (1), 61-74, 1999	463	1999
A comparison of the continuous and discrete adjoint approach to automatic aerodynamic optimization S Nadarajah, A Jameson 38th Aerospace sciences meeting and exhibit, 667, 2000	459	2000
Supercritical Wing Sections II: A Handbook, Lecture Notes in Economics and Mathematical Systems F Bauer, P Garabedian, D Korn, A Jameson Springer-Verlag, 1975	451*	1975
Iterative solution of transonic flows over airfoils and wings, including flows at Mach 1 A Jameson Communications on pure and applied mathematics 27 (3), 283-309, 1974	451	1974
Multigrid solution of the Navier-Stokes equations on triangular meshes DJ Mavriplis, A Jameson AIAA journal 28 (8), 1415-1425, 1990	426	1990
A new class of high-order energy stable flux reconstruction schemes PE Vincent, P Castonguay, A Jameson Journal of Scientific Computing 47, 50-72, 2011	421	2011
Implicit schemes and 𝐿𝑈 decompositions A Jameson, E Turkel Mathematics of Computation 37 (156), 385-397, 1981	384	1981
Aerodynamic shape optimization using the adjoint method A Jameson Lectures at the Von Karman Institute, Brussels, 2003	368	2003

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