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Evaluation of a Second-Order Accurate Navier-Stokes Code for Detached Eddy Simulation Past a Circular CylinderWe evaluate the applicability of a production computational fluid dynamics code for conducting detached eddy simulation for unsteady flows. A second-order accurate Navier-Stokes code developed at NASA Langley Research Center, known as TLNS3D, is used for these simulations. We focus our attention on high Reynolds number flow (Re = 5 x 10(sup 4) - 1.4 x 10(sup 5)) past a circular cylinder to simulate flows with large-scale separations. We consider two types of flow situations: one in which the flow at the separation point is laminar, and the other in which the flow is already turbulent when it detaches from the surface of the cylinder. Solutions are presented for two- and three-dimensional calculations using both the unsteady Reynolds-averaged Navier-Stokes paradigm and the detached eddy simulation treatment. All calculations use the standard Spalart-Allmaras turbulence model as the base model.
Document ID
20040013487
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Vatsa, Veer N.
(NASA Langley Research Center Hampton, VA, United States)
Singer, Bart A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2003
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
AIAA Paper 2003-4085
Report Number: AIAA Paper 2003-4085
Meeting Information
Meeting: 21st AIAA Applied Aerodynamics Conference
Location: Orlando, FL
Country: United States
Start Date: June 23, 2003
End Date: June 26, 2003
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
OTHER: RTA 781-10-11-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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