Velocity effects in transverse mode liquid propellant rocket combustion instability-Reference-Cited by-同舟云学术

Velocity effects in transverse mode liquid propellant rocket combustion instability

Published:1964-09 Issue:9 Volume:2 Page:1631-1641
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

REARDON F. H.¹,CROCCO L.¹,HARRJE D. T.¹

Affiliation:

1. Princeton University, Princeton, N. J.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.2631

Reference15 articles.

1. Transverse Combustion Instability in Liquid Propellant Rocket Motors

2. Scala, S. M. "Transverse wave and entropy wave combustion instability in liquid propellant rockets/5Princeton Univ., Ph.D. Thesis,Aeronautical Engineering Rept. 380 (April 1957).

3. Theory of Liquid PropelIant Rocket Combustion Instability and Its Experimental Verification

4. Reardon, F. H. "An investigation of transverse mode combustion instability in liquid propellant rocket motors," Princeton Univ., Ph.D. Thesis,Aeronautical Engineering Rept. 550 (June 1961).

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