Acoustic-instability boundaries in liquid-propellant rockets: Theoretical explanation of empirical correlation

Journal of Propulsion and Power

Volumn 12, Issue 3, 1996, Pages 621-624

  Kim, J S ^a,b   Williams, F A ^a,b,c  

^a UNIVERSITY OF CALIFORNIA   (United States)

^b Dept Appl Mechanics and Eng Sci

^c AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC WAVES; AMPLIFICATION; COMBUSTION; CORRELATION METHODS; FLAME RESEARCH; LIQUID PROPELLANTS; REACTION KINETICS; STABILITY; STRAIN RATE;

ACOUSTIC INSTABILITY BOUNDARIES; CHAMBER PRESSURE; COUNTERFLOW FLAMELET RESPONSE MODEL; FLAME RESPONSE ANALYSIS; HEWITT STABILITY CORRELATION; IMPINGING JET INJECTORS; LIQUID PROPELLANT ROCKETS;

ROCKET ENGINES;

EID: 0030144637     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/3.24081     Document Type: Article

References (14)

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