Flow-Structure Interaction Simulations for Ballutes in Supersonic Flow
Author:
Affiliation:
1. Louisiana State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-2906
Reference12 articles.
1. On the calculation of flow past axisymmetric bodies with detached shock waves using an electronic computing machine
2. Testing of Flexible Ballutes in Hypersonic Wind Tunnels for Planetary Aerocapture
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