Wall shear stress and heat transfer for shock- induced laminar boundary layers.
- 1 August 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (8), 1620-1621
- https://doi.org/10.2514/3.4833
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- On the laminar compressible boundary layer induced by the passage of a plane shock wave over a flat wallMathematical Proceedings of the Cambridge Philosophical Society, 1967
- On the laminar compressible boundary layer with stationary origin on a moving flat wallMathematical Proceedings of the Cambridge Philosophical Society, 1967
- Viscosity of Dissociated Gases from Shock-Tube Heat-Transfer MeasurementsPhysics of Fluids, 1961