Interaction between a conical shock wave and a plane turbulent boundary layer

AIAA journal

Volumn 38, Issue 5, 2000, Pages 804-811

  Gai, S L ^a   Teh, S L ^b  

^a School of Engineering and Information Technology   (Australia)

^b NANYANG TECHNOLOGICAL UNIVERSITY   (Singapore)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; CONES; FLOW PATTERNS; FLOW VISUALIZATION; PLATES (STRUCTURAL COMPONENTS); PRESSURE MEASUREMENT; REYNOLDS NUMBER; SCHLIEREN SYSTEMS; SHOCK WAVES; SUPERSONIC AERODYNAMICS; TURBULENT FLOW; WIND TUNNELS;

CONICAL SHOCK WAVE; CROSSFLOWS; FLOW SEPARATION; PRESSURE GRADIENTS;

FLOW INTERACTIONS;

EID: 0034188161     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1060     Document Type: Article

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