Hypersonic Reentry Vehicle Wake Flow Fields at Angle of Attack-Reference-Cited by-同舟云学术

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Hypersonic Reentry Vehicle Wake Flow Fields at Angle of Attack

Published:2006-01-09 Issue: Volume: Page:
ISSN:
Container-title:44th AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Lin Tony¹,Sproul Linda¹,Kim Moon¹,Olmos M¹,Feiz H¹

Affiliation:

1. Northrop Grumman Corporation

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-582

Reference48 articles.

1. 1Martelluci,A."ExperimentalStudyofNearWakes,"BSD-TR-67-229-Vol.1.DataPresentation, November1967.

2. 3Conti,Raul,"NumericalMethodforBaseandWakeFlowAnalysis,"DET10TR94-22,January

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1. Computation of aerodynamic coefficients of a re-entry vehicle at Mach 6;ADV AIRCR SPACECR SC;2023

2. Impact of angle of attack on plasma flow and electromagnetic wave propagation around hypersonic vehicles;Microwave and Optical Technology Letters;2020-06

3. Understanding of flow features over a typical crew module at Mach 4;The Aeronautical Journal;2015-06

4. Control of High-Angle-of-Attack Reentry Flow with Plasma Actuators;Journal of Spacecraft and Rockets;2013-03

5. Hypersonic Flow Computations for an Elliptic Cone at High Angle of Incidence;Journal of Spacecraft and Rockets;2012-05

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