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Lag Model Predictions for UFAST SBLI FlowfieldPresentation for Shock Boundary Layer Interaction Workshop. Shows results for Lag turbulence model on one of the international workshop test cases the UFAST 8 degree test case. Comparison with PIV velocity measurements as well as computed tunnel wall flowfields are shown, emphasizing that the interaction is a 3D phenomena, and is reasonably well predicted.
Document ID
20100027328
Acquisition Source
Ames Research Center
Document Type
Other
Authors
Olsen, Mike (NASA Ames Research Center Moffett Field, CA, United States)
Lillard, Randy (NASA Johnson Space Center Houston, TX, United States)
Oliver, Brandon (NASA Johnson Space Center Houston, TX, United States)
Blaisdell, Gregory (Purdue Univ. West Lafayette, IN, United States)
Date Acquired
August 24, 2013
Publication Date
February 26, 2010
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
ARC-E-DAA-TN1241
Report Number: ARC-E-DAA-TN1241
Distribution Limits
Public
Copyright
Public Use Permitted.

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