Implicit Large-Eddy Simulations of Zero-Pressure Gradient, Turbulent Boundary LayerA set of direct simulations of zero-pressure gradient, turbulent boundary layer flows are conducted using various span widths (62-630 wall units), to document their influence on the generated turbulence. The FDL3DI code that solves compressible Navier-Stokes equations using high-order compact-difference scheme and filter, with the standard recycling/rescaling method of turbulence generation, is used. Results are analyzed at two different Re values (500 and 1,400), and compared with spectral DNS data. They show that a minimum span width is required for the mere initiation of numerical turbulence. Narrower domains ((is) less than 100 w.u.) result in relaminarization. Wider spans ((is) greater than 600 w.u.) are required for the turbulent statistics to match reference DNS. The upper-wall boundary condition for this setup spawns marginal deviations in the mean velocity and Reynolds stress profiles, particularly in the buffer region.
Document ID
20150023002
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)
Date Acquired
December 15, 2015
Publication Date
January 4, 2015
Subject Category
Aerodynamics
Report/Patent Number
ARC-E-DAA-TN19819Report Number: ARC-E-DAA-TN19819
Meeting Information
Meeting: AIAA SciTech 2015
Location: Kissimmee, FL
Country: United States
Start Date: January 4, 2015
End Date: January 8, 2015
Sponsors: American Inst. of Aeronautics and Astronautics