Transient Three-Dimensional Side Load Analysis of Out-of-Round Film Cooled Nozzles-Reference-Cited by-同舟云学术

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Transient Three-Dimensional Side Load Analysis of Out-of-Round Film Cooled Nozzles

Published:2010-07-25 Issue: Volume: Page:
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Container-title:46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Wang Ten-See,Lin Jeff,Ruf Joseph,Guidos Michael

Publisher

American Institute of Aeronautics and Astronautics

Reference15 articles.

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

2. Waves - An International Journal on Shock Waves, Detonations and Explosions. Vol. 19, Issue 3, 2009, pp. 251~264. DOI:

3. Journal of PropulsionandPower, Vol.25, No. 6, 2009. DOI:10.2514/1.41025.10.2514/1.41025

4. Ostland, J. "Supersonic Flow Separation with Application to Rocket Engine Nozzles," Doctoral Thesis,Royal Institute

Cited by 1 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. Modeling Free Shock Separation Induced Side Loads in Overexpanded Rocket Nozzles;AIAA Journal;2015-01

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