Verification Test Suite for Spalart-Allmaras QCR2000 Turbulence Model
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Computational Aerodynamics, verification, Spallart↗
Engineering topics
Stephen L. Wood
Publications and source records attributed to Stephen L. Wood.
Verification Test Suite for Spalart-Allmaras QCR2000 Turbulence Model
The paper presents three benchmark cases for verification of Reynolds-averaged Navier-Stokes solvers. The verification studies focus on a one-equation Spalart-Allmaras model, SA-[neg]-QCR2000, that uses a version of quadratic constitutive relations.The benchmark cases are a two-dimensional subsonic flow around a Joukowski airfoil, a three-dimensional supersonic flow through a square duct, and a three-dimensional flow over a wing-fuselage configuration. The turbulence-model formulation, geometry, flow conditions, grids, and the expected output are described in detail. Reference solutions computed by several established codes are shown
Computational Aerodynamics↗
Angle-of-Attack Sweep with Mesh Adaptation for High-Lift Configurations
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High-lift CRM Mesh Adaptation RANS↗
Anisotropic Goal-Based Mesh Adaptation Metric Clarification and Development
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adjoint goal mesh adaptation metric stabilized fin↗