Experimental and numerical study of heat flux in dual bell nozzles-Reference-Cited by-同舟云学术

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Experimental and numerical study of heat flux in dual bell nozzles

Published:2011-07-31 Issue: Volume: Page:
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Container-title:47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Génin Chloe,Gernoth Andreas,Stark Ralf

Publisher

American Institute of Aeronautics and Astronautics

Reference8 articles.

1. 2Horn, M. and Fisher, S. Dual-Bell Altitude Compensating Nozzles, NASA-CR-194719, 1994.

2. 3Hagemann, G., Immich, H., Van Nguyen, T. and Dumnov, G. Advanced Rocket Nozzles, Journal of Propulsion and Power, 1998.

3. 6Stark, R. and Hagemann, G. Current status of numerical flow prediction for separated nozzle flows, 2nd European Conference for Aerospace Sciences (EUCASS), Brussels, Belgium, 1-6July, 2007.

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1. Application of a partitioned field approach to transient aerothermal problems in rocket nozzles;Computers & Fluids;2013-12

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