Flowrate and acoustics characteristics of coaxial swirling injector of hydrogen/oxygen rocket engine-Reference-Cited by-同舟云学术

Flowrate and acoustics characteristics of coaxial swirling injector of hydrogen/oxygen rocket engine

Published:1996-07-01 Issue: Volume: Page:
ISSN:
Container-title:32nd Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Zhou Jin¹,Hu Xiaoping¹,Huang Yuhui¹,Wang Zhenguo¹

Affiliation:

1. National Univ. of Defense Technology, Changsha, China

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-3135

Reference5 articles.

1. Ghafourian A., Mahalingam S., Dindi H. and Daily I W., AReview of Atomization in Liquid RocketEngines,AIAA91-0283,1991

2. Xiaoping Hu, Jin Zhou, Zhenguo Wang and Liangsheng Zhong, Experimental Studies on Atomization and flux Distributions of Gas-Liquid CoaxialInjectors, AIAA96-3023,1996

3. JingxiangWu, WeidongLiu,FengchenZhuang, Studies on Large Flux Coaxial Injector Spray Modelandatomization,AIAA 93-2160

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