Flow over a biconic configuration with an afterbody compression flap- A comparative numerical study
- 12 July 1983
- 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 wing-fuselage aerodynamic interactionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- An efficient method for supersonic viscous flow field calculationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983