Experimental and numerical investigations of nozzle geometry effect on the instabilities in solid propellant boosters

36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2000, Pages

  Anthoine, J ^a   Buchlin, J M ^a   Guery, J F ^b  

^a VON KARMAN INSTITUTE FOR FLUID DYNAMICS   (Belgium)

^b Le Bouchet Research Center   (France)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC TRANSDUCERS; BOOSTERS (ROCKET); POLYCHLORINATED BIPHENYLS; PROPULSION; ROCKET NOZZLES; SOLID PROPELLANTS;

ACOUSTIC MEASUREMENTS; ACOUSTIC PRESSURES; COLD FLOW MODELING; FLOW-ACOUSTIC COUPLING; NUMERICAL INVESTIGATIONS; RECIRCULATION BUBBLES; RESONANCE AMPLITUDES; SOLID-PROPELLANT BOOSTERS;

NOZZLE DESIGN;

EID: 85087594593     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-3560     Document Type: Conference Paper

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