Simulation of transonic viscous flow over a fighter-like configuration including inlet
- 8 June 1987
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Impingement of an oblique shock wave on a cylinderPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Numerical solution of supersonic laminar flow over an inclined body of revolutionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- On implicit finite-difference simulations of three-dimensional flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978