Computational simulation improvements of supersonic high-angle-of-attack missile flows

Journal of Spacecraft and Rockets

Volumn 36, Issue 1, 1999, Pages 59-66

  Josyula, Eswar ^a,b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b Computational Sciences Branch ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; DIFFERENCE EQUATIONS; INTEGRATION; MATHEMATICAL MODELS; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER; SHOCK WAVES; STEADY FLOW; SUPERSONIC FLOW; TURBULENT FLOW; VISCOUS FLOW; VORTEX FLOW;

ANGLE OF ATTACK; GRID RESOLUTION ANALYSIS; MACH NUMBER;

MISSILES;

EID: 0032735808     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3433     Document Type: Article

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