Supersonic Parachute Aerodynamic Testing and Fluid Structure Interaction Simulation
Abstract
The ESA Supersonic Parachute program expands the knowledge of parachute inflation and flying characteristics in supersonic flows using wind tunnel testing and fluid structure interaction to develop new inflation algorithms and aerodynamic databases.
- Publication:
-
11th International Planetary Probe Workshop
- Pub Date:
- June 2014
- Bibcode:
- 2014LPICo1795.8082L