Application of the direct simulation Monte Carlo method to the full shuttle geometry
- 18 June 1990
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Hypersonic rarefied flow about plates at incidencePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989