Measurement and Calculation of Shock Stand-off Distances over Hypersonic Spheres in CO2-Reference-Cited by-同舟云学术

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Measurement and Calculation of Shock Stand-off Distances over Hypersonic Spheres in CO2

Published:2017-03-02 Issue: Volume: Page:
ISSN:
Container-title:21st AIAA International Space Planes and Hypersonics Technologies Conference
language:
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Author:

Liao Dongjun¹,Liu Sen¹,Jian Hexiang¹,Xie Aimin¹,Wang Zonghao¹,Huang Jie¹

Affiliation:

1. China Aerodynamics Research and Development Center

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2017-2124

Reference24 articles.

1. Mark, S., McNeil, C., and Prasun, D. "Static Aerodynamic of the Mars Exploration Rover Entry Capsule," AIAA 2005-0056.

2. Furudate, M., Suzuki, T., Takayanagi, H., and Fujita, K. "Three Dimensional Aerodynamics Study for Mars Aeroshell in NonequilibriumFlow," AIAA 2010-4647,2010.

3. Artem, D., Mark, S., and John, N. "Hypersonic and Supersonic Static Aerodynamics of Mars Science Laboratory Entry Vehicle," AIAA 2012-2999,2012

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