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The widely used turbulence model, called k-ω SST, can give rise to some numerical problems due to the associated boundary condition for ω on the walls. We propose a modification of the model, which gives virtually identical results to the original model, but with a boundary condition that meets the numerical requirements.

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This page is a summary of: The k−ω Shear Stress Transport Model with ω=0 at the Wall, AIAA Journal, August 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j066004.
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