Computational and experimental investigation of a nonslender delta wing

AIAA Journal

Volumn 47, Issue 8, 2009, Pages 1811-1825

  Gordnier, Raymond E ^a,c   Visbal, Miguel R ^a,c   Gursul, Ismet ^b,d   Wang, Zhijin ^b,d  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b UNIVERSITY OF BATH   (United Kingdom)

^c Computational Sciences Branch ^*  (United States)

^d Department of Mechanical Engineering ^*

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL SIMULATION; DELTA WINGS; DIFFERENCE SCHEMES; EXPERIMENTAL INVESTIGATIONS; GRID POINTS; GRID RESOLUTION; HIGH RESOLUTION; HIGH-ORDER ACCURACY; HIGHER ORDER; IMPLICIT LARGE EDDY SIMULATIONS; INSTANTANEOUS FLOW; LEADING EDGE; NONSLENDER DELTA WINGS; NUMERICAL RESULTS; PARTICLE IMAGE VELOCIMETRIES; SEPARATED FLOWS; SURFACE BOUNDARY-LAYER; SURFACE FLOW; SYMMETRY PLANES; TURBULENCE MODELING; VORTEX BREAKDOWN; VORTICAL FLOWS;

ATMOSPHERIC THERMODYNAMICS; COMPUTATIONAL FLUID DYNAMICS; DELTA WING AIRCRAFT; DIFFERENCE EQUATIONS; FLOW VISUALIZATION; LARGE EDDY SIMULATION; REFINING; REYNOLDS NUMBER; SYSTEMS ENGINEERING;

NAVIER STOKES EQUATIONS;

EID: 69949183619     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.37848     Document Type: Article

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