Stabilized Finite Elements in FUN3DA Streamlined Upwind Petrov-Galerkin (SUPG) stabilized finite-element discretization has been implemented as a library into the FUN3D unstructured-grid flow solver. Motivation for the selection of this methodology is given, details of the implementation are provided, and the discretization for the interior scheme is verified for linear and quadratic elements by using the method of manufactured solutions. A methodology is also described for capturing shocks, and simulation results are compared to the finite-volume formulation that is currently the primary method employed for routine engineering applications. The finite-element methodology is demonstrated to be more accurate than the finite-volume technology, particularly on tetrahedral meshes where the solutions obtained using the finite-volume scheme can suffer from adverse effects caused by bias in the grid. Although no effort has been made to date to optimize computational efficiency, the finite-element scheme is competitive with the finite-volume scheme in terms of computer time to reach convergence.
Document ID
20170001235
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Anderson, W. Kyle (NASA Langley Research Center Hampton, VA, United States)
Newman, James C. (Tennessee Univ. Chattanooga, TN, United States)
Karman, Steve L. (Pointwise, Inc. Fort Worth, TX, United States)
Date Acquired
February 2, 2017
Publication Date
January 9, 2017
Subject Category
Fluid Mechanics And ThermodynamicsNumerical AnalysisComputer Programming And Software
Report/Patent Number
NF1676L-24680Report Number: NF1676L-24680
Meeting Information
Meeting: 2017 AIAA Science and Technology Forum and Exposition (SciTech)
Location: Grapevine, TX
Country: United States
Start Date: January 9, 2017
End Date: January 13, 2017
Sponsors: American Inst. of Aeronautics and Astronautics