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- W2230862521 abstract "To investigate the effect of viscosity on the transition to Mach reflexion in pseudosteady flow, the Reynolds number of the flow behind the reflected shock was varied by changing the shock tube initial pressure. A model developed to describe the viscous effect on transition predicted a linear dependence of the observed transition angle on Re -1/2. Experiments at a shock Mach number of 5.4 demonstrated this behaviour." @default.
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- W2230862521 date "1980-01-01" @default.
- W2230862521 modified "2023-09-27" @default.
- W2230862521 title "The Effect of Viscosity on the Transition to Mach Reflexion in Pseudosteady Flow" @default.
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