Further experiments on spreading of liquids injected into a supersonic flow.
Author:
Affiliation:
1. The Aerospace Corporation, El Segundo, Calif.
2. Naval Postgraduate School, Monterey, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference6 articles.
1. Study of penetration of a liquid injectant into a supersonic flow.
2. Breakup rate and penetration of a liquid jet in a gas stream.
3. Study of liquid jet penetration in a hypersonic stream
Cited by 9 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. Droplet breakup phenomena in flows with velocity lag;Progress in Energy and Combustion Science;1996-01
2. Modeling of liquid jets injected transversely into a supersonic crossflow;AIAA Journal;1989-12
3. Effects of properties and location in the plume on droplet diameter for injection in a supersonic stream;AIAA Journal;1983-07
4. Mean droplet diameter resulting from atomization of a transverse liquid jet in a supersonic air stream;International Meeting and Technical Display on Global Technology 2000;1980-05-06
5. Penetration and Breakup of Liquids in Subsonic Airstreams;AIAA Journal;1977-10
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