Compressible Viscous Flow Past a Wedge Moving at Hypersonic Speeds
- 1 April 1956
- journal article
- research article
- Published by Wiley in Journal of Mathematics and Physics
- Vol. 35 (1-4) , 179-193
- https://doi.org/10.1002/sapm1956351179
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Viscous Flow Along a Flat Plate Moving at High Supersonic SpeedsJournal of the Aeronautical Sciences, 1956
- Shock-Wave Effects on the Laminar Skin Friction of an Insulated Flat Plate at Hypersonic SpeedsJournal of the Aeronautical Sciences, 1953
- On Weak Interaction of Strong Shock and Mach Waves Generated Downstream of the ShockJournal of the Aeronautical Sciences, 1952
- An Estimate of Viscosity Effect on the Hypersonic Flow Over an Insulated WedgeJournal of Mathematics and Physics, 1952
- Temperature and Velocity Profiles in the Compressible Laminar Boundary Layer with Arbitrary Distribution of Surface TemperatureJournal of the Aeronautical Sciences, 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