Large eddy simulation of stable supersonic jet impinging on flat plate

AIAA Journal

Volumn 48, Issue 10, 2010, Pages 2325-2338

  Dauptain, A ^a,b   Cuenot, B ^a,b   Gicquel, L Y M ^a,b  

^a Centre Européen Research et de Formation Avencée en Calcul Scientifique   (France)

^b NONE

Author keywords

[No Author keywords available]

Indexed keywords

EXPERIMENTAL DATA; FLAT PLATE; FLOW INDUCED; GRID-INDEPENDENT; HIGH VELOCITY; MESH REFINEMENT; NUMERICAL DISSIPATION; NUMERICAL STUDIES; PRESSURE FIELD; RECIRCULATION ZONES; ROOT-MEAN-SQUARE PRESSURE; SHEAR LAYER; SMAGORINSKY MODEL; SPECTRAL CONTENT; SUPERSONIC JETS; THIRD-ORDER; TURBULENT VISCOSITY; TWO-POINT; TWO-POINT CORRELATION FUNCTION; UNSTRUCTURED MESHES; WALL PRESSURE;

ATMOSPHERIC BOUNDARY LAYER; INCOMPRESSIBLE FLOW; LARGE EDDY SIMULATION; MESH GENERATION; SUPERSONIC AERODYNAMICS;

COMPUTER SIMULATION;

EID: 78649623949     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.J050362     Document Type: Article

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