Boundary-layer transition measurements in hypervelocity flows in a shock tunnel

AIAA Journal

Volumn 40, Issue 8, 2002, Pages 1542-1548

  Mee, David J ^a  

^a UNIVERSITY OF QUEENSLAND   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

ELECTROMAGNETIC WAVE ATTENUATION; ENTHALPY; GAGES; HEAT TRANSFER; REYNOLDS NUMBER; SHOCK TUBES; SURFACE ROUGHNESS; THIN FILMS; TURBULENCE;

SHOCK TUNNELS;

BOUNDARY LAYERS;

EID: 0036684904     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1851     Document Type: Article

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