Combustion Instability Mechanisms in a Pressure-coupled Gas-gas Coaxial Rocket Injector

Author:

Harvazinski Matthew E.1,Huang Cheng2,Sankaran Venkateswaran1,Feldman Thomas2,Anderson William2,Merkle Charles2,Talley Doug G.1

Affiliation:

1. Air Force Research Laboratory

2. Purdue University

Publisher

American Institute of Aeronautics and Astronautics

Reference38 articles.

1. 1Harrje, D. and Reardon, F. “Liquid Propellant Rocket Combustion Instability,” Technical Report SP-194, NASA, Washington D.C., 1972.

2. Combustion instabilities - Mating dance of chemical, combustion, and combustor dynamics

3. Combustion Dynamics and Instabilities: Elementary Coupling and Driving Mechanisms

4. 4Culick, F. “Combustion Instabilities in Liquid-Fueled Propulsion Systems an Overview,” Tech. Rep. CP-450, AGARD, 1989.

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