The Effect of Prandtl Number on the Theoretical Shock-Wave Thickness
- 1 April 1951
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 18 (4) , 286-287
- https://doi.org/10.2514/8.1933
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- An Extension of the Theory of the One-Dimensional Shock-Wave StructureJournal of the Aeronautical Sciences, 1950