Computational study of a turbulent delta-wing flowfield using two-equation turbulence models

1996 Fluid Dynamics Conference

Volumn , Issue , 1996, Pages 1-23

  Gordnier, Raymond E ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DELTA WING AIRCRAFT; REYNOLDS NUMBER; TURBULENCE MODELS; WINGS;

ALGEBRAIC TURBULENCE MODELING; BALDWIN LOMAX MODEL; COMPUTATIONAL RESULTS; COMPUTATIONAL STUDIES; HIGH REYNOLDS NUMBER; QUANTITATIVE ACCURACY; TWO-EQUATION TURBULENCE MODELS; VORTEX BREAKDOWN;

VORTEX FLOW;

EID: 84959220720     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-2076     Document Type: Conference Paper

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