What is it about?
Natural-laminar-flow (NLF) wings provide the potential to significantly reduce the fuel burn of transport aircraft. We present methods for the efficient prediction of laminar-turbulent boundary-layer transition that will accelerate the analysis and optimization of NLF wing designs
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This page is a summary of: Smooth Local Correlation-Based Transition Model for the Spalart–Allmaras Turbulence Model, AIAA Journal, October 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j059784.
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