Computational fluid dynamic studies of a solid and ribbon 12-gore parachute canopy in subsonic and supersonic flow
- 15 May 1995
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- A new solution method for steady-state canopy structural loadsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Parametric Study of Parachute Pressure Distribution by Wind Tunnel TestingJournal of Aircraft, 1976