The Shock Strength in a Two-Dimensional Nonsteady Flow
- 1 May 1952
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 19 (5) , 351-352
- https://doi.org/10.2514/8.2280
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Strength of Reflected Shock in Mach ReflectionJournal of the Aeronautical Sciences, 1951
- Aerodynamics of BlastsJournal of the Aeronautical Sciences, 1951
- CX. The shock strength in supersonic “conical fields.”Journal of Computers in Education, 1949
- CIX. A Technique for rendering approximate solutions to physical problems uniformly validJournal of Computers in Education, 1949