Enthalpy effects on hypervelocity boundary-layer transition: Ground test and flight data

Journal of Spacecraft and Rockets

Volumn 34, Issue 5, 1997, Pages 614-619

  Adam, Philippe H ^a,b   Hornung, Hans G ^a,b  

^a CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; ENTHALPY; HYPERSONIC AERODYNAMICS; REYNOLDS NUMBER;

HYPERVELOCITY SHOCK TUNNELS;

TRANSITION FLOW;

EID: 0031223033     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3278     Document Type: Article

References (18)

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