Reverse Flow Solutions for Compressible Laminar Boundary-Layer Equations
- 1 March 1969
- journal article
- conference paper
- Published by AIP Publishing in Physics of Fluids
- Vol. 12 (3) , 517-523
- https://doi.org/10.1063/1.1692514
Abstract
Several new similarity solutions are presented for the laminar compressible boundary layer with reverse flow for Prandtl numbers of 1.0 and 0.723. New solutions without reverse flow are presented for Prandtl number equal 0.723. Wall-to-stagnation temperature ratios from 0 to 2 are considered. These solutions quantitatively show the effects of pressure gradient, and wall heat transfer on the wall shearing stress and enthalpy gradient.Keywords
This publication has 4 references indexed in Scilit:
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- Similarity Solutions for the Compressible Laminar Boundary Layer with Heat and Mass TransferPhysics of Fluids, 1967
- Supersonic separated and reattaching laminar flows. i - general theory and application to adiabatic boundary-layershock-wave interactionsAIAA Journal, 1964
- Wake-like solutions of the laminar boundary- layer equationsAIAA Journal, 1964