Numerical Simulation of a Supersonic Cruise Nozzle-Reference-Cited by-同舟云学术

Numerical Simulation of a Supersonic Cruise Nozzle

Published:2013-01-05 Issue: Volume: Page:
ISSN:
Container-title:51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Sasanapuri Balasubramanyam¹,Kumar Manish¹,Wirogo Sutikno¹,Kurbatskii Konstantin¹

Affiliation:

1. ANSYS, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-492

Reference24 articles.

1. ANSYS, Inc. Product Documentation Release 14.5,ANSYS, Inc., Canonsburg, PA15317,USA, 2012.

2. 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.

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

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

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