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High‐order strand grid methods for low‐speed and incompressible flows
Authors:Jonathan Thorne  Aaron Katz  Oisin Tong  Yushi Yanagita  Yoshiharu Tamaki  Keegan Delaney
Affiliation:1. Department of Mechanical and Aerospace Engineering, Utah State University, Logan, UT, USA;2. Department of Aeronautics and Astronautics, University of Tokyo, Tokyo, Japan;3. Computational Hydromechanics Division, NSWCCD, West Bethesda, MD, USA
Abstract:A novel high‐order finite volume scheme using flux correction methods in conjunction with structured finite differences is extended to low Mach and incompressible flows on strand grids. Flux correction achieves a high order by explicitly canceling low‐order truncation error terms across finite volume faces and is applied in unstructured layers of the strand grid. The layers are then coupled together using a source term containing summation‐by‐parts finite differences in the strand direction. A preconditioner is employed to extend the method to low speed and incompressible flows. We further extend the method to turbulent flows with the Spalart–Allmaras model. Laminar flow test cases indicate improvements in accuracy and convergence using the high‐order preconditioned method, while turbulent body‐of‐revolution flow results show improvements in only some cases, perhaps because of dominant errors arising from the turbulence model itself. Copyright © 2016 John Wiley & Sons, Ltd.
Keywords:preconditioning  strand grids  high‐order methods  incompressible flows
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