Assessment and Extension of the WrayAgarwal Turbulence Model for Shock WaveBoundary Layer Interactions

Date

2024-01-01

Author

Akça, Semih Can
Dikbaş, Erdem
Baran, Özgür Uğraş

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This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

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In this study, the performance of the Wray-Agarwal one-equation turbulence model is evaluated using Shock Wave-Boundary Layer Interaction (SWBLI) test cases. Also, a recently tested formulation by Raje and Sinha aiming for enhancement in SWBLI flow predictions for the k-ω SST model is applied to the Wray-Agarwal turbulence model as an extension. By introducing Reynolds stress anisotropy to the turbulent boundary layer, an updated version of the Wray-Agarwal model is proposed. The modified version of the model is tested using supersonic and hypersonic compression ramps and impinging shock-type flow problems. It is shown that the current extended version of the model predicts the shock-induced separation locations more accurately than the standard Wray-Agarwal model for compression ramptype flow problems. The modifications have no significant effect on the predictions of impinging shock-type problems.

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https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=85203286442&origin=inward
https://hdl.handle.net/11511/111206

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Department of Mechanical Engineering, Conference / Seminar