Analysis of combustion instability via constant volume combustion in a LOX/RP-1 bipropellant liquid rocket engine

Author:

Zhang HuiQiang,Ga YongJing,Wang Bing,Wang XiLin

Publisher

Springer Science and Business Media LLC

Subject

General Engineering,General Materials Science

Reference31 articles.

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2. Habiballah M, Dubois I. Numerical analysis of engine instability. In: Yang V, Anderson W, eds. Liquid Rocket Engine Combustion Instability, Progress in Astronautics and Aeronautics, NASA. Washington D C: American Institute of Aeronautics and Astronautics, 1995, 169: 475–502

3. Hulka J, Hutt J J. Instability phenomena in a liquid oxygen/hydrogen propellant rocket engines. In: Yang V, Anderson W, eds. Liquid Rocket Engine Combustion Instability, Progress in Astronautics and Aeronautics, NASA. Washington D C: American Institute of Aeronautics and Astronautics, 1995, 169: 39–72

4. Lambiris S, Combs L P, Levine R S. Stable combustion processes in liquid propellant rocket engines. In: Combustion and Propulsion Fifth AGARD Colloquium. Braunschweig, 1962

5. Strahle W C. Unsteady laminar jet flame at large frequencies of oscillation. AIAA J, 1965, 3(5): 957–960

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