Computational algorithms for aerodynamic analysis and design

Applied Numerical Mathematics

Volumn 13, Issue 5, 1993, Pages 383-422

  Jameson, Antony ^a  

^a PRINCETON UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 38248999778     PISSN: 01689274     EISSN: None     Source Type: Journal    
DOI: 10.1016/0168-9274(93)90096-A     Document Type: Article

References (29)

1. Construction of TVD-like artificial viscosities on 2-dimensional arbitrary FEM grids
2. Flux corrected transport, 1 SHASTA, a fluid transport algorithm that works
3. On the numerical solution of nonlinear problems in fluid dynamics by least squares and finite element methods (II): application to transonic flow simu lations
4. Computers vs. wind tunnels in aerodynamic flow simulations
5. Computers vs. wind tunnels in aerodynamic flow simulations
6. A special stability problem for linear multistep methods
7. An improved time marching method for turbomachinery flow calculations
8. The numerical integration of stiff ordinary differential equations
9. High resolution schemes for hyperbolic conservation laws
10. Iterative solution of transonic flows over airfoils and wings including flows at Mach 1
11. Acceleration of transonic potential flow calculations on arbitrary meshes by the multiple grid method
12. Solution of the Euler equations by a multigrid method
13. A non-oscillatory shock capturing scheme using flux limited dissipation
14. Multigrid algorithms for compressible flow calculations
15. Successes and challenges in computational aerodynamics
16. Aerodynamic design via control theory
17. Automatic design of transonic airfoils to reduce the shock induced pressure drag
18. Time dependent calculations using multigrid, with applications to unsteady flows past airfoils and wings
19. Calculation of invisoid transonic flow over a complete aircraft
20. Numerical solutions of the Euler equations by finite volume methods with Runge-Kutta time stepping schemes
21. Extremum control II: semi-discrete approximations to conservation laws
22. A new method of two dimensional aerodynamic design
23. A new flux splitting scheme
24. Validation of a multigrid method for the Reynolds averaged equations
25. Approximate Riemann solvers, parameter vectors, and difference schemes
26. Flux vector splitting of the inviscid gas dynamic equations with applications to finite difference methods
27. On central-difference and upwind schemes