Effect of propellant morphology on acoustics in a planar rocket motor

Theoretical and Computational Fluid Dynamics

Volumn 23, Issue 1, 2009, Pages 63-77

  Daimon, Y ^a   Jackson, T L ^a   Topalian, V ^a   Freund, J B ^a   Buckmaster, J ^b  

^a UNIVERSITY OF ILLINOIS AT URBANA CHAMPAIGN   (United States)

^b Buckmaster Research   (United States)

Author keywords

Acoustics; Fluid dynamics; Heterogeneous propellants; Numerical simulations; Solid rocket motor

Indexed keywords

ASYMPTOTIC SOLUTIONS; HETEROGENEOUS PROPELLANTS; HIGH ORDERS; LONGITUDINAL ACOUSTIC MODES; MASS INJECTIONS; NUMERICAL SIMULATIONS; NUMERICAL SOLVERS; ROCKET MOTORS; SOLID ROCKET MOTOR; TIME DEPENDENTS; TWO-DIMENSIONAL;

COMPUTER SIMULATION; FLUID DYNAMICS; MATHEMATICAL MODELS; MOTORS; PROPELLANTS; ROCKET ENGINES; ROCKETS; SPACECRAFT PROPULSION; WHITE NOISE;

ACOUSTICS;

ACOUSTICS; FLUID DYNAMICS; MORPHOLOGY; NUMERICAL MODEL;

EID: 62249125460     PISSN: 09354964     EISSN: 14322250     Source Type: Journal    
DOI: 10.1007/s00162-008-0089-y     Document Type: Article

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