RTO WG 10: Test cases for CFD validation of hypersonic flight

40th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2002, Pages

  Knight, Doyle ^a  

^a RUTGERS UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; COMPUTATIONAL FLUID DYNAMICS; HYPERSONIC AERODYNAMICS; HYPERSONIC VEHICLES; LAMINAR BOUNDARY LAYER; SHOCK WAVES; TWO PHASE FLOW;

BOUNDARY LAYER INSTABILITY; CFD METHODOLOGIES; EFFECTIVE ANALYSIS; HYPERSONIC FLIGHTS; RESEARCH TECHNOLOGY ORGANIZATIONS; SHOCK-SHOCK INTERACTIONS; TURBULENT BOUNDARY-LAYER INTERACTIONS; VISCOUS-INVISCID INTERACTION;

HYPERSONIC BOUNDARY LAYERS;

EID: 85085404959     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-433     Document Type: Conference Paper

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