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- W4317633410 abstract "This paper describes the problem setup, implementation, and numerical results obtained with the commercial CFD software ANSYS Fluent to test the accuracy of the one-equation Wray-Agarwal (WA) turbulence model in comparison to the commonly used one-equation Spalart-Allmaras (SA) turbulence model by computing two axisymmetric benchmark problems, namely the subsonic flow past an axisymmetric after-body and the transonic flow past Sandia axisymmetric bump. The axisymmetric after-body case features low speed flow in near separation conditions where it was found that the Wray-Agarwal model and the Spalart-Allmaras model produced nearly identical results. The Sandia transonic axisymmetric bump case features a complex flow in which shock induced separation occurs over the geometry. In this test case the Wray-Agarwal model was seen to improve accuracy over the Spalart-Allmaras model in terms of pressure distribution and separation prediction on the bump." @default.
- W4317633410 created "2023-01-21" @default.
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- W4317633410 date "2023-01-19" @default.
- W4317633410 modified "2023-09-30" @default.
- W4317633410 title "Application of Wray-Agarwal Turbulence Model to Axisymmetric Subsonic and Transonic Flows" @default.
- W4317633410 cites W2121125723 @default.
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- W4317633410 doi "https://doi.org/10.2514/6.2023-1614" @default.
- W4317633410 hasPublicationYear "2023" @default.
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