The thermal nature of the triple point of a Mach reflection

G. Ben-Dor, K. Takayama, C. E. Needham

Research output: Contribution to journalArticlepeer-review

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 languageEnglish
Pages (from-to)1287-1293
JournalPhysics of Fluids
Volume30
DOIs
StatePublished - 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

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