Abstract
The interaction of a planar shock wave with a high density layer (low
temperature or low speed of sound) has been investigated both
numerically and analytically. It has been shown that depending on the
incident shock wave Mach number, M(sub s), and the densities ratio
across the interface, rho(sub 4)/rho(sub 0), the interaction results in
either a stationary regular reflection, RR, or a stationary Mach
reflection, MR. However, even when a stationary RR is established, it is
preceded by a transient MR. In addition it has been proven that the
RR-MR reversible transition takes place at the normal shock point, i.e.,
the mechanical-equilibrium condition. Finally the interaction has been
simulated with and without viscous effects, and as a result the effect
of viscosity was clarified.
Original language | English |
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Title of host publication | Proceedings of the International Workshop on Strong Shock Waves |
Pages | 145-164 |
State | Published - 1 Mar 1992 |
Externally published | Yes |
Keywords
- Boundary Layers
- Gases
- Mach Reflection
- Shock Wave Interaction
- Shock Wave Propagation
- Shock Waves
- Viscosity
- Angles (Geometry)
- Boundary Conditions
- Computerized Simulation
- Fluid Dynamics
- Fluid Flow
- Iteration
- Mach Number