Flow Separation Studies in a Subscale Truncated Ideal Contour Nozzle-Reference-Cited by-同舟云学术

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Flow Separation Studies in a Subscale Truncated Ideal Contour Nozzle

Published:2007-01-08 Issue: Volume: Page:
ISSN:
Container-title:45th AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Verma Shashi¹,Haidn Oskar²

Affiliation:

1. National Aerospace Laboratories

2. DLR, German Aerospace Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-1320

Reference18 articles.

1. C.A. Hunter,``Experimental, Theoretical and Computational Investigation of Separated Nozzle Flows'', AIAA 98-3107.

2. Terhardt, M., Hagemann, G., and Frey, M. "Flow Separation and Side-Load Behaviour in the Vulcain Engine", AIAA 99-2762.

3. R. Schmucker. Flow Processes in Overexpanded Nozzles of Chemical Rocket Engines. Report TB-7-10-14, TechnicalUniversity, Munich,July1973.

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1. Theories and methods for designing hypersonic high-enthalpy flow nozzles;Chinese Journal of Aeronautics;2022-01

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