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Hybrid RANS/LES methodologies are at the forefront of modern CFD with the ability to obtain high-fidelity solutions with the need for a full, computationally prohibitive LES. Here different and new hybrid methods are implemented and compared in the NASA Langley code Overflow.

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This page is a summary of: Application of Hybrid Reynolds Averaged Navier–Stokes and Large-Eddy-Simulation Eddy Viscosity Blending Methods in OVERFLOW, AIAA Journal, November 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j060398.
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