Aerodynamic analysis of finned missiles at supersonic speeds and high angles of attack

18th Applied Aerodynamics Conference

Volumn , Issue , 2000, Pages

  Kinsey, Don W ^a   Strang, William Z ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; COMPUTATIONAL FLUID DYNAMICS; FINS (HEAT EXCHANGE); FLOW PATTERNS; MACH NUMBER; MISSILES; NASA; REYNOLDS NUMBER; SUPERSONIC AIRCRAFT; TURBULENCE MODELS; VORTEX FLOW;

AERODYNAMIC ANALYSIS; AERODYNAMIC CHARACTERISTICS; COMPUTATIONAL SOLUTIONS; FLIGHT CONDITIONS; HIGH ANGLES OF ATTACK; HIGH REYNOLDS NUMBER; SHARP LEADING EDGES; SUPERSONIC SPEED;

VERTICAL STABILIZERS;

EID: 85085402575     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-4213     Document Type: Conference Paper

References (10)

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8. Grismer M. J., Strang, W. Z., Tomaro, R. F., and Witzeman, F. C., "Cobalt60: A Parallel, Implicit, Unstructured Euler/Navier-Stokes Solver, "Advances in Engineering Software, Vol 29, No. 3-6, pp. 365-373, Apr-Jun 1998.
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