Study of LOx/H2 Spray Flame Response to Acoustic Excitation in a Rectangular Rocket Combustor-Reference-Cited by-同舟云学术

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Study of LOx/H2 Spray Flame Response to Acoustic Excitation in a Rectangular Rocket Combustor

Published:2013-07-12 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
language:
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Author:

Hardi Justin¹,Oschwald Michael¹,Dally Bassam B.²

Affiliation:

1. German Aerospace Center (DLR)

2. University of Adelaide

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-3781

Reference46 articles.

1. Yang,V.,andAnderson,W.E., eds.,Liquidrocketenginecombustioninstability,AIAA,Washington,DC,1995.

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