Validation of transient cooling modeling for hypersonic application

Journal of Thermophysics and Heat Transfer

Volumn 21, Issue 1, 2007, Pages 86-94

  Gascoin, Nicolas ^a,c,d   Gillard, Philippe ^a,c   Dufour, Emmanuel ^b   Touré, Youssoufi ^a,e  

^a UNIVERSITÉ D'ORLÉANS   (France)

^b MBDA FRANCE   (France)

^c Lab Energetique Explosions Struct   (France)

^d AIAA   (United States)

^e Laboratoire Vision et Robotique   (France)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; HEAT FLUX; JET ENGINES; MASS TRANSFER; MATHEMATICAL MODELS;

HEAT FLUXES CONSERVATION; THERMAL BOUNDARY LAYERS;

HYPERSONIC AERODYNAMICS;

BOUNDARY LAYERS; HEAT FLUX; HYPERSONIC AERODYNAMICS; JET ENGINES; MASS TRANSFER; MATHEMATICAL MODELS;

EID: 33847082892     PISSN: 08878722     EISSN: 15336808     Source Type: Journal    
DOI: 10.2514/1.26022     Document Type: Article

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