MODE IDENTIFICATION OF HIGH-AMPLITUDE PRESSURE WAVES IN LIQUID ROCKET ENGINES-Reference-Cited by-同舟云学术

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MODE IDENTIFICATION OF HIGH-AMPLITUDE PRESSURE WAVES IN LIQUID ROCKET ENGINES

Published:2000-01 Issue:4 Volume:229 Page:973-991
ISSN:0022-460X
Container-title:Journal of Sound and Vibration
language:en
Short-container-title:Journal of Sound and Vibration

Author:

EBRAHIMI R.,MAZAHERI K.,GHAFOURIAN A.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics

Reference16 articles.

1. Combustion instability in liquid propellant rocket motors;CROCCO;Experimental Method in Combustion Research (AGARD),1963

2. R. R. WEISS, 1996, Technical Report AFRPL-TR-66-150, An introduction to combustion instability in liquid propellant rocket engines

3. D. T. HARRJE, F. H. REARDON, 1972, NASA SP-194, Liquid propellant rocket combustion instability

4. Theoretical studies on liquid propellant rocket instability;CROCCO;Tenth Symposium (International) on Combustion,1965

5. F. E. C. CULICK, 1989, AGARD Conference Proceedings No., Combustion instability in liquid-fueled propulsion systems — an overview

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