Prediction of high frequency combustion instability in liquid propellant rocket engines-Reference-Cited by-同舟云学术

Prediction of high frequency combustion instability in liquid propellant rocket engines

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

KIM Y.¹,CHEN C.¹,ZIEBARTH J.¹,CHEN Y.²

Affiliation:

1. Alabama, University, Huntsville

2. Engineering Science, Inc., Huntsville, AL

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-3763

Reference34 articles.

1. 'Sirignano, W.A. "A threoretical study of non-linear combustion instability: longitudinal mode," Princeton University AMS Technical Report So. 677,1964

2. 3Mitchell, C.E. "Axial mode shock wave combustion instability in liquid propellant rocket engines: Princeton University AMS Technical Report No. 798, 1967

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