Experimental and theoretical studies on thermoacoustic limit cycle oscillation in a simplified solid rocket motor using flat flame burner

Author:

Ma Baoyin,Li Junwei,Zhang Zhihui,Xi Yunzhi,Zhao DanORCID,Wang Ningfei

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference52 articles.

1. Dynamics and stability of lean-premixed swirl-stabilized combustion;Huang;Prog. Energy Combust. Sci.,2009

2. Pressure oscillations and instability of working processes in the combustion chambers of solid rocket motors;Emelyanov;Acta Astronaut.,2017

3. Study on instable combustion of solid rocket motor with finocyl grain;Hu Daning;China Ordnance,2011

4. F. Culick, Research on combustion instability and application to solid propellant rocket motors, in: 7th Propulsion Joint Specialist Conference.

5. Calculation of acoustic admittance at a burning surface;Ryazantsev;Acta Astronaut.,1976

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