Low Reynolds Number Effects in a Mach 3 Shock / Turbulent-Boundary-Layer Interaction

@inproceedings{Ringuette2008LowRN,
  title={Low Reynolds Number Effects in a Mach 3 Shock / Turbulent-Boundary-Layer Interaction},
  author={Marc Ringuette and Minwei Wu and M. Pino Mart{\'i}n},
  year={2008}
}
Cf = skin-friction coefficient Lsep = separation length M = freestream Mach number Re = Reynolds number based on T = temperature u = velocity in the streamwise direction v = velocity in the spanwise direction w = velocity in the wall-normal direction = 99% thickness of the incoming boundary layer = displacement thickness of the incoming boundary layer = ratio of to the wall unit = momentum thickness of the incoming boundary layer = density 
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