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Application of CFD to Abrupt Wing Stall Using RANS and DESFor DES, RANS is responsible for predicting boundary layer growth and separation. LES is responsible for predicting the geometry dependent turbulent flow features. Grid adaptation done using NASA Langley s RefineMesh program. Adaptation on time average of vorticity
Document ID
20040086519
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Forsythe, Jim (Cobalt Solutions, LLC Springfield, OH, United States)
Date Acquired
September 7, 2013
Publication Date
April 1, 2004
Publication Information
Publication: COMSAC: Computational Methods for Stability and Control, Part 2
Subject Category
Fluid Mechanics And Thermodynamics
Funding Number(s)
CONTRACT_GRANT: NAS1-00135
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle20040086515Collected WorksCOMSAC: Computational Methods for Stability and Control20040086515Collected WorksCOMSAC: Computational Methods for Stability and Control
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