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An Upwind Solver for the National Combustion CodeAn upwind solver is presented for the unstructured grid National Combustion Code (NCC). The compressible Navier-Stokes equations with time-derivative preconditioning and preconditioned flux-difference splitting of the inviscid terms are used. First order derivatives are computed on cell faces and used to evaluate the shear stresses and heat fluxes. A new flux limiter uses these same first order derivatives in the evaluation of left and right states used in the flux-difference splitting. The k-epsilon turbulence equations are solved with the same second-order method. The new solver has been installed in a recent version of NCC and the resulting code has been tested successfully in 2D on two laminar cases with known solutions and one turbulent case with experimental data.
Document ID
20110012000
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Sockol, Peter M.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
January 4, 2011
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
E-17651
Report Number: E-17651
Meeting Information
Meeting: 49th Aerospace Sciences Meeting
Location: Orlando, FL
Country: United States
Start Date: January 4, 2011
End Date: January 7, 2011
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 561581 ,02,08.03.16.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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