Transient Three-Dimensional Startup Side Load Analysis of a Regeneratively Cooled Nozzle-Reference-Cited by-同舟云学术

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Transient Three-Dimensional Startup Side Load Analysis of a Regeneratively Cooled Nozzle

Published:2008-06-15 Issue: Volume: Page:
ISSN:
Container-title:38th Fluid Dynamics Conference and Exhibit
language:
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Author:

Wang Ten-See¹

Affiliation:

1. NASA Marshall Space Flight Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-4300

Reference29 articles.

1. Sea level side loads in high-area-ratio rocket engines

2. 2Cikanek,H.A."CharacteristicsofSpaceShuttleMainEngineFailures,"AIAAPaper87-1939,June1987.

3. Measurement ofFluid/StructureInteraction,"AIAAPaper 2002-3999, July2002.

4. Journal of PropulsionandPower, Vol.19, No. 3, 2003,pp.321-331.

5. Paper2002-3841, July2002.

Cited by 3 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 investigation of flow separation behavior in an over-expanded annular conical aerospike nozzle;Chinese Journal of Aeronautics;2015-08

2. Robust non-reflecting boundary conditions for the simulation of rocket nozzle flow;Aerospace Science and Technology;2010-09

3. Nozzle flow separation;Shock Waves;2009-06-06

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