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https://doi.org/10.2514/3.49207
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Cite Journal: AIAA Journal |  Publication Date: Feb 1, 1974 |
 Citations: 12 |
A proposed method for calculating three-dimensional incompressible laminar and turbulent boundary layers is investigated with respect to its applicability to incompressible attachment line flow on an infinite swept wing. The calculation results obtained exhibit satisfactory agreement with experimental data.
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