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Streamlined Convergence Acceleration for CFD CodesEnigma, a simplified interface to the PETSc library, is shown to enable the rapid solution of discrete partial differential equations. Two CFD codes, LAURA and HyperSolve, use Enigma to compute steady solutions of the Navier-Stokes equations. Using PETSc, Enigma is shown to provide a Jacobian-Free Newton-Krylov method (JFNK), globalized with pseudotransient continuation, that improves efficiency over the point-implicit relaxation method traditionally used by LAURA. It is shown that iterative error has a large impact on surface heat transfer predicted by LAURA on an axisymmetric sphere-cone geometry. Also, the convergence rate of HyperSolve simulating subsonic flow over a delta wing geometry with the JFNK method is shown to be more efficient than employing a defect correction method as the nonlinear solver.
Document ID
20200002615
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Thompson, Kyle B.
(NASA Langley Research Center Hampton, VA, United States)
O'Connell, Matthew D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
April 17, 2020
Publication Date
June 17, 2019
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NF1676L-31505
Report Number: NF1676L-31505
Meeting Information
Meeting: AIAA Aviation Forum 2019
Location: Dallas, TX
Country: United States
Start Date: June 17, 2019
End Date: June 21, 2019
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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