The transition of planar shock waves over straight wedges in steady flows between regular and Mach reflection was numerically studied by the DSMC method for small Knudsen numbers. The hysteresis effect was observed at increasing and decreasing shock wave angle. Stability of regular and Mach reflecti
Technical noteOn the stability of steady–flow regular and Mach reflection
✍ Scribed by H.G. Hornung
- Publisher
- Springer-Verlag
- Year
- 1997
- Tongue
- English
- Weight
- 619 KB
- Volume
- 7
- Category
- Article
- ISSN
- 0938-1287
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