Compact difference scheme applied to simulation of low-sweep delta wing flow

AIAA Journal

Volumn 43, Issue 8, 2005, Pages 1744-1752

  Gordnier, Raymond E ^a,b   Visbal, Miguel R ^a,b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b Air Vehicles Directorate   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; CONVERGENCE OF NUMERICAL METHODS; LOW PASS FILTERS; NAVIER STOKES EQUATIONS;

COMPACT DIFFERENCE SCHEME; DELTA WINGS; VORTEX BREAKDOWN; VORTEX STRUCTURES;

VORTEX FLOW;

EID: 24144451842     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.5403     Document Type: Article

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