Numerical Simulation on Supersonic Aerodynamic Interference for Rigid and Flexible Parachutes
Author:
Affiliation:
1. Nagoya University
2. Mitsubishi Heavy Industries, Ltd.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-3269
Reference16 articles.
1. Results from the Mars Science Laboratory Parachute Decelerator System Supersonic Qualification Program
2. 4Barnhardt, M.D. "Modeling and Simulation of High-speed Wake Flows," Ph.D. Dissertation,University of Minnesota, 2009.
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