Supersonic nonlinear potential flow with subsonic regions and implicit isentropic shock fitting
- 23 June 1981
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Nonlinear Supersonic Potential Flow over Delta WingsAIAA Journal, 1981
- Opportunities for supersonic performance gains through non-linear aerodynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- A study of the inviscid flow about conically cambered delta wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Iterative solution of transonic flows over airfoils and wings, including flows at mach 1Communications on Pure and Applied Mathematics, 1974