Adiabatic Wall Solutions for the Hypersonic Compressible Laminar Boundary-Layer Equations
- 1 May 1970
- journal article
- Published by AIP Publishing in Physics of Fluids
- Vol. 13 (5) , 1142-1145
- https://doi.org/10.1063/1.1693043
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Further similar laminar-flow solutions.AIAA Journal, 1969
- Reverse Flow Solutions for Compressible Laminar Boundary-Layer EquationsPhysics of Fluids, 1969
- The behaviour of a laminar compressible boundary layer near a point of zero skin-frictionJournal of Fluid Mechanics, 1962