Numerical Simulation of Interaction of a Supersonic Flow over a Re-entry Vehicle with a Counterflowing Jet-Reference-Cited by-同舟云学术

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Numerical Simulation of Interaction of a Supersonic Flow over a Re-entry Vehicle with a Counterflowing Jet

Published:2012-01-09 Issue: Volume: Page:
ISSN:
Container-title:50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Kumar Manish¹,Devaki RaviKumar¹,Wirogo Sutikno¹,Kurbatskii Konstantin¹

Affiliation:

1. ANSYS, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-863

Reference27 articles.

1. Dynamics of Shock Dispersion and Interactions in Supersonic Freestreams with Counterflowing Jets

2. ANSYS,Inc.ProductDocumentationRelease13.0,ANSYS,Inc.,Canonsburg,PA15317,USA,2010.

3. Tamada, I., Aso, S., and Tani, Y. "Numerical Study of the Effect of the Opposing Jet on Reduction of Aerodynamic Heatingwith Different NoseConfigurations," AIAA Paper2005-188,2005.

4. Flowfield Around Spike-Tipped Bodies for High Attack Angles at Mach 4.5

5. Venkateswaran, S., Weiss, J. M., and Merkle, C. L. "Propulsion Related Flowfields Using the Preconditioned Navier-StokesEquations,"AIAApaper92-3437.

Cited by 2 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. Numerical prediction of mean flow and acoustic field of a supersonic impinging jet;International Journal of Aeroacoustics;2024-05-09

2. Sensitivity analysis of flowfield modeling parameters upon the flow structure and aerodynamics of an opposing jet over a hypersonic blunt body;Chinese Journal of Aeronautics;2020-01

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