Parametric Study on Aerodynamic Interaction of Supersonic Parachute System
Author:
Affiliation:
1. Department of Aerospace Engineering, Nagoya University, Nagoya 4648603, Japan
2. Department of Mechanical Engineering, The Hong Kong Polytechnic University, Hong Kong, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053824
Reference17 articles.
1. Simulation of Parachute Fluid Structure Interaction in Supersonic Flow
2. LingardJ.DarleyM.UnderwoodJ. C. “Simulation of Mars Supersonic Parachute Performance and Dynamics,” AIAA Paper 2007-2507, 2007.
3. Detached Eddy Simulations of the MSL Parachute at Supersonic Conditions
4. Simulation of Fluid-Structure Interaction of the Mars Science Laboratory Parachute
5. Comparison of Fluid-Structure Interaction Simulations of the MSL Parachute With Wind Tunnel Tests
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