RTO WG 10: CFD validation for shock wave turbulent boundary layer interactions

40th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2002, Pages

  Knight, Doyle ^a   Yan, Hong ^a   Panaras, Argyris ^b   Zheltovodov, Alexander ^c  

^a RUTGERS UNIVERSITY   (United States)

^b NATIONAL TECHNICAL UNIVERSITY OF ATHENS   (Greece)

^c KHRISTIANOVICH INSTITUTE OF THEORETICAL AND APPLIED MECHANICS   (Russian Federation)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; COMPUTATIONAL FLUID DYNAMICS; FINS (HEAT EXCHANGE); HYPERSONIC VEHICLES; LAMINAR BOUNDARY LAYER; LARGE EDDY SIMULATION; NAVIER STOKES EQUATIONS; NOZZLE DESIGN; SHOCK WAVES; TURBULENCE;

BOUNDARY LAYER TRANSITIONS; COMPRESSION CORNERS; PLUME INTERACTION; REYNOLDS-AVERAGED NAVIER-STOKES SIMULATIONS; SCRAMJET PROPULSION; SHOCK-SHOCK INTERACTIONS; TURBULENT BOUNDARY-LAYER INTERACTIONS; VISCOUS-INVISCID INTERACTION;

ATMOSPHERIC THERMODYNAMICS;

EID: 85084460995     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-437     Document Type: Conference Paper

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