Experimental investigation of the flow structure near a single wraparound fin

Journal of Spacecraft and Rockets

Volumn 34, Issue 6, 1997, Pages 729-736

  Tilmann, C P ^a,d   Huffman Jr , R E ^a,d   Buter, T A ^b,d   Bowersox, R D W ^c,d  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

^c Box 870280   (United States)

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANEMOMETERS; BOUNDARY LAYERS; FINS (HEAT EXCHANGE); FLOW PATTERNS; MATHEMATICAL MODELS; NUMERICAL METHODS; PROBES; REYNOLDS NUMBER; SHEAR STRESS; SUPERSONIC FLOW; TURBULENCE;

CROSS WIRE HOT FILM ANEMOMETRY; FLOW STRUCTURE; MACH NUMBER; SHOCK BOUNDARY LAYER INTERACTION; SINGLE WRAPAROUND FIN;

HYPERSONIC FLOW;

EID: 0031270175     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3303     Document Type: Article

References (14)

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