LE-7A Engine Nozzle Flow Separation Phenomena and a Method of RSS Suppression with a Step inside Nozzle-Reference-Cited by-同舟云学术

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LE-7A Engine Nozzle Flow Separation Phenomena and a Method of RSS Suppression with a Step inside Nozzle

Published:2007 Issue:645 Volume:55 Page:474-482
ISSN:1344-6460
Container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:ja
Short-container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Author:

Watanabe Yasuhide,Sakazume Norio,Yonezawa Kouichi,Tsujimoto Yoshinobu

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/jjsass/55/645/55_645_474/_pdf

Reference13 articles.

1. 1) Frey, M. and Hagemann, G.: Flow Separation and Side-Loads in Rocket Nozzles, AIAA Paper 99-2815, 1999.

2. 2) Watanabe, Y., Sakazume, N. and Tsuboi, M.: LE-7A Engine Nozzle Problems during the Transient Operations, AIAA Paper 2002-3841, 2002.

3. 3) Watanabe, Y., Sakazume, N. and Tsuboi, M.: LE-7A Engine Nozzle Separation Phenomenon during the Transient Process, ISTS 2002-a-24, 2002.

4. 4) Yonezawa, K., Yokota, K., Tsujimoto, Y., Watanabe, Y. and Abe, T.: 2-D Numerical Simulation of Side Loads in Rocket Nozzles, ISTS 2002-e-27, 2002.

Cited by 2 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. Investigation of conjugate circular arcs in rocket nozzle contour design;Shock Waves;2018-05-28

2. Control of the asymmetric flow in rocket nozzles;Journal of Thermal Science;2013-03-28

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