Shock wave/transitional boundary-layer interactions in hypersonic flow

AIAA Journal

Volumn 44, Issue 6, 2006, Pages 1243-1254

  Benay, R ^a   Chanetz, B ^a   Mangin, B ^a   Vandomme, L ^a   Perraud, J ^a,b  

^a ONERA   (France)

^b Toulouse Center   (France)

Author keywords

[No Author keywords available]

Indexed keywords

HEAT FLUX MEASUREMENTS; PITOT BOUNDARY-LAYER SURVEYS; STAGNATION PRESSURE; TRANSITIONAL BOUNDARY-LAYER INTERACTIONS;

BOUNDARY LAYERS; COMPUTER SIMULATION; HEAT FLUX; LASER DOPPLER VELOCIMETERS; PROBLEM SOLVING; REYNOLDS NUMBER; SHOCK WAVES; VORTEX FLOW;

HYPERSONIC FLOW;

EID: 33746334124     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.10512     Document Type: Article

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