Antony Jameson
Antony Jameson
Professor of Aerospace Engineering, Texas A&M University
Verified email at - Homepage
Cited by
Cited by
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
Time dependent calculations using multigrid, with applications to unsteady flows past airfoils and wings
A Jameson
10th Computational Fluid Dynamics Conference, 1596, 1991
Aerodynamic design via control theory
A Jameson
Journal of scientific computing 3 (3), 233-260, 1988
Lower-upper symmetric-Gauss-Seidel method for the Euler and Navier-Stokes equations
S Yoon, A Jameson
AIAA journal 26 (9), 1025-1026, 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
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
Supercritical Wing Sections II: A Handbook
F Bauer, P Garabedian, D Korn, A Jameson
Springer Science & Business Media, 2012
Lower-upper implicit schemes with multiple grids for the Euler equations
A Jameson, S Yoon
AIAA journal 25 (7), 929-935, 1987
Calculation of inviscid transonic flow over a complete aircraft
A Jameson, T Baker, N Weatherill
24th Aerospace Sciences Meeting, 1986
Solution of the Euler equations for complex configurations
A Jameson, T Baker
6th Computational Fluid Dynamics Conference Danvers, 1929, 1983
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
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
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
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
Optimum aerodynamic design using CFD and control theory
A Jameson
12th Computational Fluid Dynamics Conference, 1729, 1995
Multigrid solution of the Navier-Stokes equations on triangular meshes
DJ Mavriplis, A Jameson
AIAA journal 28 (8), 1415-1425, 1990
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
Implicit schemes and 𝐿𝑈 decompositions
A Jameson, E Turkel
Mathematics of Computation 37 (156), 385-397, 1981
Multigrid solution of the two-dimensional Euler equations on unstructured triangular meshes
DJ Mavriplis
AIAA journal 26 (7), 824-831, 1988
Transonic flow calculations for aircraft
A Jameson
Numerical methods in fluid dynamics, 156-242, 1985
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