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Detached Eddy Simulations of Hypersonic TransitionThis slide presentation reviews the use of Detached Eddy Simulation (DES) of hypersonic transistion. The objective of the study was to investigate the feasibility of using CFD in general, DES in particular, for prediction of roughness-induced boundary layer transition to turbulence and the resulting increase in heat transfer.
Document ID
20110011022
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Yoon, S. (NASA Ames Research Center Moffett Field, CA, United States)
Barnhardt, M. (Eloret Corp. Moffett Field, CA, United States)
Candler, G. (Minnesota Univ. Minneapolis, MN, United States)
Date Acquired
August 25, 2013
Publication Date
July 12, 2010
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
ARC-E-DAA-TN1807
Report Number: ARC-E-DAA-TN1807
Meeting Information
Meeting: 6th International Conference on Computational Fluid Dynamics (ICCFD6)
Location: St Petersburg
Country: Russia
Start Date: July 12, 2010
End Date: July 16, 2010
Funding Number(s)
CONTRACT_GRANT: NNA10DE12C
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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