NASA NTRS · 19710000154
Computing incompressible laminar and turbulent boundary layer formation
Abstract
Program generates initial laminar conditions, such as in Falkner-Skan similarity flows, or turbulent equilibrium profiles. Initial profile input data is used. Combination with inviscid-freestream calculations to predict entire flow field in turbine cascade or around airfoil is possible.
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Herring, H. J., Mellor, G. L.. 1971-05-01. Computing incompressible laminar and turbulent boundary layer formation. https://ntrs.nasa.gov/citations/19710000154
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