Transition delay in hypervelocity boundary layers by means of CO 2/acoustic instability interactions

47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition

Volumn , Issue , 2009, Pages

  Leyva, Ivett A ^a   Laurence, Stuart ^a   Beierholm, Amy War Kei ^a,b   Hornung, Hans G ^a   Wagnild, Ross ^c   Candler, Graham ^c  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

^c UNIVERSITY OF MINNESOTA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC INSTABILITY; AXISYMMETRIC; CALTECH; COMPUTATIONAL DATA; EXPERIMENTAL DATA; EXPERIMENTAL MODELS; FREE-STREAM; HEAT TRANSFER MEASUREMENTS; HYPERVELOCITIES; HYPERVELOCITY FLOW; INJECTION SCHEMES; INJECTION TIMING; MOLE FRACTION; NOVEL METHODS; NUMERICAL DATA; REFLECTED SHOCKS; SHADOWGRAPH VISUALIZATION; SLENDER BODIES; TRANSITION LOCATIONS; TRANSITION REYNOLDS NUMBER; UNIVERSITY OF MINNESOTA; VIBRATIONAL MODES;

AEROSPACE ENGINEERING; BOUNDARY LAYERS; HYPERSONIC AERODYNAMICS; PROPULSION; REYNOLDS NUMBER; THERMOCOUPLES; VISUALIZATION;

HYPERSONIC VEHICLES;

EID: 78549241986     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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