Experimental study on aerothermal heating caused by jet-hypersonic crossflow interaction

Journal of Spacecraft and Rockets

Volumn 45, Issue 5, 2008, Pages 891-899

  Gülhan, Ali ^a,b   Schütte, Gerrit ^a,c   Stahl, Bernhard ^a,b  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

^b Institute of Aerodynamic and Flow Technology   (Germany)

^c UNIVERSITY OF STUTTGART   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; ATMOSPHERIC TEMPERATURE; MISSILES; RADIATIVE COOLING; SURFACE PROPERTIES; THERMAL CONDUCTIVITY; TOPOLOGY; WALL FLOW;

AEROTHERMAL HEATING; HEAT FLUX DISTRIBUTIONS; LOW THERMAL CONDUCTIVITY; MISSILE CONFIGURATION; SURFACE TEMPERATURE DISTRIBUTION; SURFACE TEMPERATURES; TEMPERATURE-DEPENDENT MATERIAL; WALL-PRESSURE DISTRIBUTION;

HEAT FLUX;

EID: 54249154722     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/1.35899     Document Type: Article

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