Exploring Shockwave Interaction With Flame

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  • This is the density field of a shock-
  • Wind tunnel Mach numer 2.0 Boundary layer over the flat surface is thin. Ramp angle is changed from 20 to 30 degrees.
  • Shock wave interaction
  • This is an unsteady viscous computation of a shock tube problem in a closed 1x1 box. The initial conditions are set with two gases ...
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pulse comcustion. Shock- Simulation of a Shock-Flame Interaction in a Reacting Flow in CONVERGE™ Materials are being used by government certified experts, not not attempt. Disclaimer: Combustion experiments are dangerous ...

【Luftvis Schlieren】Transonic Shock Wave Boundary Layer Interaction over a Shock Generation Bump

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