The Transverse Curvature Effect in Compressible Axially Symmetric Laminar Boundary-Layer Flow
- 1 March 1956
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 23 (3), 208-224
- https://doi.org/10.2514/8.3537
Abstract
No abstract availableThis publication has 14 references indexed in Scilit:
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- Temperature and Velocity Profiles in the Compressible Laminar Boundary Layer with Arbitrary Distribution of Surface TemperatureJournal of the Aeronautical Sciences, 1949
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