Higher mean-flow approximation for solid rocket motors with radially regressing walls

AIAA Journal

Volumn 40, Issue 9, 2002, Pages 1780-1788

  Majdalani, Joseph ^a   Vyas, Anand B ^a   Flandro, Gary A ^b  

^a Marquette University   (United States)

^b UNIVERSITY OF TENNESSEE SPACE INSTITUTE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC FIELDS; APPROXIMATION THEORY; BOUNDARY LAYERS; DIFFERENTIAL EQUATIONS; INCOMPRESSIBLE FLOW; NAVIER STOKES EQUATIONS; NONLINEAR EQUATIONS; PERTURBATION TECHNIQUES; PROPELLANTS; REYNOLDS NUMBER; TURBULENCE; VISCOUS FLOW;

RADIALLY REGRESSING WALLS;

ROCKET ENGINES;

EID: 0036712506     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1854     Document Type: Article

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