The effect of aspect ratio on the effectiveness of combustor coolantpassages-Reference-Cited by-同舟云学术

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The effect of aspect ratio on the effectiveness of combustor coolantpassages

Published:1992-07-06 Issue: Volume: Page:
ISSN:
Container-title:28th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

YAGLEY J.¹,FENG J.¹,MERKLE C.¹,LEE Y.-T.²

Affiliation:

1. Pennsylvania State University, University Park

2. U.S. Navy, David Taylor Research Center, Bethesda, MD

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-3153

Reference13 articles.

1. Frohlich,A, Irnmich. H., Lebail,F.andPopp,M. "Three-dimensionalFlowAnalysisinA Rocket EngineCoolantChannelof HighDepthAnJidth Ratio",27thJoint PropulsionConference,AlAA Paper 91-2183,June, 1991,Sacramento,Ca.

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