Abstract
The paper deals with an analytical and experimental study aimed at
clarifying the problem of reflection of oblique shock waves in unsteady
monatomic and diatomic gas flows. The analysis shows that for incident
shock Mach numbers in the range from 1 to 10, there exist seven
diffraction domains in nitrogen and six domains in argon, all of which
are composed of the four well-known regular reflections, single-Mach
reflection, complex-Mach reflection, and double-Mach reflection.
Real-gas effects are shown to affect significantly both the transition
boundaries between the reflections and the domain dimensions. The
analytical results are in complete agreement with hypersonic shock tube
experiments.
Original language | English |
---|---|
Title of host publication | Proceedings of the Twelfth International Symposium |
Pages | 288-297 |
State | Published - 1980 |
Externally published | Yes |
Keywords
- Boundary Layer Transition
- Gas Flow
- Mach Reflection
- Oblique Shock Waves
- Unsteady Flow
- Argon
- Density Distribution
- Diatomic Gases
- Domains
- Monatomic Gases
- Nitrogen
- Shock Tubes
- Wave Diffraction
- Wave Reflection