On the Interaction of a Plane Shock Wave with a Wedge
- 1 July 1954
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 21 (7) , 501-504
- https://doi.org/10.2514/8.3103
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- Compressible Laminar Boundary Layer on a Heat-Insulated BodyJournal of the Aeronautical Sciences, 1953
- On Heat Transfer, Recovery Factors, and Spin for Laminar FlowsJournal of the Aeronautical Sciences, 1952
- Ein Quadraturverfahren zur Berechnung der laminaren und turbulenten Reibungsschicht bei ebener und rotationssymmetrischer Str mungArchive of Applied Mechanics, 1952
- Approximate Calculation of the Laminar Boundary LayerAeronautical Quarterly, 1949
- Temperature and Velocity Profiles in the Compressible Laminar Boundary Layer with Arbitrary Distribution of Surface TemperatureJournal of the Aeronautical Sciences, 1949
- On Two‐Dimensional Non‐Steady Motion of a Slender Body in a Compressible FluidJournal of Mathematics and Physics, 1948
- Anwendung des Energiesatzes von Wieghardt auf einparametrige Geschwindigkeitsprofile in laminaren GrenzschichtenArchive of Applied Mechanics, 1948