The Compressible Laminar Boundary Layer with Arbitrary Pressure and Surface Temperature Gradients
- 1 December 1953
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 20 (12) , 805-818
- https://doi.org/10.2514/8.2866
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
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- Steady flow in the laminar boundary layer of a gasProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1949
- Temperature and Velocity Profiles in the Compressible Laminar Boundary Layer with Arbitrary Distribution of Surface TemperatureJournal of the Aeronautical Sciences, 1949
- Some remarks on the flat plate boundary layerQuarterly of Applied Mathematics, 1949
- Concerning the effect of compressibility on lam inar boundary layers and their separationProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1948
- The laminar boundary layer in compressible flowPhilosophical Transactions of the Royal Society of London. Series A, Mathematical and Physical Sciences, 1948
- On the nature of the boundary layer near the leading edge of a flat plateQuarterly of Applied Mathematics, 1948