Boundary layer transition measurements in hypervelocity flows in a shock tunnel

39th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2001, Pages

  Mee, David J ^a  

^a UNIVERSITY OF QUEENSLAND   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; ATMOSPHERIC THERMODYNAMICS; ENTHALPY; HEAT TRANSFER; REYNOLDS NUMBER;

BOUNDARY LAYER TRANSITIONS; HYPERVELOCITIES; HYPERVELOCITY FLOW; TEST SURFACES; THIN FILM HEAT TRANSFER; TRANSFER SIGNALS; TRANSITION LOCATIONS; TURBULENT SPOTS;

LAMINAR BOUNDARY LAYER;

EID: 85043778883     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-208     Document Type: Conference Paper

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