Experimental and numerical study of the Mars Sample Return Orbiter in cold laminar hypersonic flow-Reference-Cited by-同舟云学术

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Experimental and numerical study of the Mars Sample Return Orbiter in cold laminar hypersonic flow

Published:2002-02 Issue:2 Volume:6 Page:115-121
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Chanetz B.,Pot T.,Le Sant Y.,Leplat M.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference14 articles.

1. Experimental and numerical study of the laminar separation in hypersonic flow;Chanetz;Aerospace Science and Technology,1998

2. Shock wave boundary layer interaction analyzed in the R5Ch wind tunnel;Chanetz;Aerospace Research,1993

3. Study of the Mars Sample Return Orbiter in the hypersonic wind tunnel R5Ch;Chanetz,2001

4. Aérothermique de l'Orbiter du programme Mars Premier en phase d'aérocapture autour de Mars;Charbonnier,2000

5. Hypersonic Flow Theory;Hayes,1959

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Prediction of the flow field over an orbiter entering the Mars atmosphere;Shock Waves;2010-01-26

2. Experimental and numerical study of the Mars Pathfinder vehicle;Aerospace Science and Technology;2003-10

3. Experimental Fluid Dynamics Technology;AIAA International Air and Space Symposium and Exposition: The Next 100 Years;2003-03-11

4. A HV pulse generator for driving pulsed corona discharge;2004 23rd IEEE Convention of Electrical and Electronics Engineers in Israel

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