Abstract
An experimental investigation followed by some theoretical
considerations suggests that the triple point of a three-shock
confluence behaves as a 'hot spot'. Numerical calculations using the
HULL code, which was developed by the U.S. Air Force Weapons Laboratory
and modified by 'S-Cubed' have provided supporting evidence for hot-spot
behavior near the triple point. Furthermore, the numerical calculations
also show a spike in the internal energy, the pressure, and the density
near the triple point.
| Original language | English |
|---|---|
| Pages (from-to) | 1287-1293 |
| Journal | Physics of Fluids |
| Volume | 30 |
| DOIs | |
| State | Published - 1 May 1987 |
Keywords
- Mach Reflection
- Shadowgraph Photography
- Shock Wave Propagation
- Temperature Effects
- Carbon Dioxide
- Computerized Simulation
- Nitrogen
- Numerical Flow Visualization
- Shock Tubes
- Wedge Flow
Fingerprint
Dive into the research topics of 'The thermal nature of the triple point of a Mach reflection'. Together they form a unique fingerprint.Cite this
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver