Three-dimensional hypersonic laminar boundary-layer computations for transition experiment design

Journal of Spacecraft and Rockets

Volumn 34, Issue 4, 1997, Pages 409-415

  Kimmel, Roger L ^a,c   Klein, Mark A ^a,c   Schwoerke, Stephen N ^b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b LOCKHEED MARTIN   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER AIDED ANALYSIS; COMPUTER SOFTWARE; CORRELATION METHODS; HYPERSONIC FLOW; LAMINAR FLOW; NAVIER STOKES EQUATIONS; NOSE CONES; REYNOLDS NUMBER; SPECTRUM ANALYSIS; TRANSITION FLOW; WIND TUNNELS;

CROSSFLOW INSTABILITY; LINEAR STABILITY THEORY; STATIONARY CROSSFLOW FACTOR; TRAVELING WAVE FACTOR;

BOUNDARY LAYER FLOW;

EID: 0031186560     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3236     Document Type: Article

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