Dependence of Shock-Tube Boundary Layers on Shock Strength
- 1 August 1969
- journal article
- Published by AIP Publishing in Physics of Fluids
- Vol. 12 (8) , 1723-1725
- https://doi.org/10.1063/1.1692732
Abstract
Using familiar considerations of vorticity transport, the essential behavior of shock‐tube boundary layers is explicitly exhibited; the nearly constant functions that cannot be calculated analytically are evaluated numerically and compared with Mirels' correlations.Keywords
This publication has 5 references indexed in Scilit:
- The transverse curvature effect on the incompressible laminar boundary layer for longitudinal flow over a cylinderZeitschrift für angewandte Mathematik und Physik, 1968
- Correlation Formulas for Laminar Shock Tube Boundary LayerPhysics of Fluids, 1966
- Test Time in Low-Pressure Shock TubesPhysics of Fluids, 1963
- SOLUTION OF THE INCOMPRESSIBLE LAMINAR BOUNDARY-LAYER EQUATIONSAIAA Journal, 1963
- On Flow Duration in Low-Pressure Shock TubesPhysics of Fluids, 1960