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Implicit LES of Turbulent, Separated Flow: Wall-Mounted Hump ConfigurationDirect simulations (ILES) of turbulent, separated flow over the wall-mounted hump configuration is conducted to investigate the physics of separated flows. A chord-based Reynolds number of Re(sub c) = 47,500 is set up, with a turbulent in flow of Re(sub theta) = 1,400 (theta/c = 3%). FDL3DI, a code that solves the compressible Navier-Stokes equations using high- order compact-difference scheme and filter, with the standard recycling/rescaling method of turbulence generation, is used. Two different configurations of the upper-wall are analyzed, and results are compared with both a higher Re(sub c) (= 936,000, Re(sub theta) = 7,200, theta/c = 0.77%) experiment for major flow features, and RANS (k-omega SST) results. A lower Rec allows for DNS-like mesh resolution, and an adequately wide span. Both ILES and RANS show delayed reattachment compared to experiment, and significantly higher skin friction in the forebody of the hump, as expected. The upper-wall shape influences the C(sub p) distribution only. Results from this study are being used to setup higher Rec (lower theta/c) ILES.
Document ID
20160002246
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Sekhar, Susheel
(Oak Ridge Associated Universities Moffett Field, CA, United States)
Mansour, Nagi N.
(NASA Ames Research Center Moffett Field, CA United States)
Caubilla, David Higuera
(Toulouse Univ. France)
Date Acquired
February 24, 2016
Publication Date
January 5, 2015
Subject Category
Aerodynamics
Fluid Mechanics And Thermodynamics
Report/Patent Number
ARC-E-DAA-TN20167
Report Number: ARC-E-DAA-TN20167
Meeting Information
Meeting: AIAA SciTech 2015
Location: Kissimmee, FL
Country: United States
Start Date: January 5, 2015
End Date: January 9, 2015
Sponsors: Toulouse Univ.
Funding Number(s)
CONTRACT_GRANT: NNH06CC03B
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Implicit LES
separated flow
Turbulent
Wall-mounted hump
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