Computational design aspects of a NASP nozzle/afterbody experiment
- 9 January 1989
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Numerical simulation of unsteady, viscous, high-angle-of-attack flows using a partially flux-split algorithmPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Normal shock location in underexpanded gas and gas-particle jetsAIAA Journal, 1964