Viscous jetting and Mach stem bifurcation in shock reflections: experiments and simulations
S. S.-M. Lau-Chapdelaine, Q. Xiao, and M. I. Radulescu

TL;DR
This study combines experiments and simulations to investigate shock reflection phenomena, revealing how variations in Mach number, Reynolds number, and isentropic exponent influence Mach stem bifurcation and vortex formation, with implications for detonation structures.
Contribution
It provides new experimental and simulation data on shock reflection, identifying the conditions under which Mach stem bifurcation occurs and its relation to flow parameters and detonation patterns.
Findings
Bifurcation occurs at low isentropic exponents and high Mach/Reynolds numbers.
Kelvin-Helmholtz instabilities cause large-scale mixing behind the Mach stem.
Maximum isentropic exponent for bifurcation is approximately 1.3.
Abstract
Shock reflection experiments are performed to study the large-scale convective mixing created by the forward jetting phenomenon. Experiments are performed at a wedge angle of in nitrogen, propane-oxygen, and hexane with incident shock Mach numbers up to . Experiments are complimented by shock-resolved viscous simulations of triple point reflection in hexane for to . Inviscid simulations are performed over a wider range of parameters. Reynolds numbers up to are covered by simulations and Reynolds numbers of are covered by experiments. The study shows that as the isentropic exponent is lowered, and as the Mach number and Reynolds number are increased, the forward jet approaches the Mach stem, forms a vortex, deforms the shock front and in some cases bifurcates the Mach stem. Experiments show…
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