A Mach 2 inflow with a split ramp configuration with an offset shows upstream flame front movement ahead of the expansion corner of the ramp. Multistep CFD simulations on HPC cluster using OpenFOAM.
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Flame flashback in supersonic flowfields
Amardip Ghosh #Advanced Propulsion Systems (APSYS) Lab
A Mach 2 inflow with a split ramp configuration with an offset shows upstream flame front movement ahead of the expansion corner of the ramp. Multistep CFD simulations on HPC cluster using OpenFOAM.