New solution method for steady-state canopy structural loads
- 1 November 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 25 (11) , 1045-1051
- https://doi.org/10.2514/3.45701
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Parametric Study of Parachute Pressure Distribution by Wind Tunnel TestingJournal of Aircraft, 1976
- Stress analysis of ribbon parachutesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Stress Analysis of Parachutes Using Finite ElementsJournal of Spacecraft and Rockets, 1971