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Shock Wave Interactions: A CFD Study of CUBRC LENS-II Turbulent ExperimentsResults of flow simulations of turbulent shock wave boundary layer interaction experiments performed in the LENS-II tunnel at CUBRC.
Document ID
20150020809
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Prabhu, Dinesh K. (ERC, Inc. Moffett Field, CA, United States)
Date Acquired
November 4, 2015
Publication Date
June 20, 2014
Subject Category
Physics (General)
Fluid Mechanics And Thermodynamics
Report/Patent Number
ARC-E-DAA-TN15585
Report Number: ARC-E-DAA-TN15585
Meeting Information
Meeting: AIAA Aviation and Aeronautics Forum and Exposition
Location: Atlanta, GA
Country: United States
Start Date: June 16, 2014
End Date: June 20, 2014
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNA10DE12C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Turbulent flow
Computational Fluid Dynamics
Reflected shock tunnel

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