supersonic flat plate -- CFD Online Discussion Forums

June 14, 2016, 02:47	supersonic flat plate	#1
Iqrar.Raza New Member Iqrar Raza Join Date: Mar 2016 Posts: 10 Rep Power: 10	Hello, I am solving a problem "supersonic flow over a flat plate ". I want ask that what should be the value of Re(L) in order to find the thickness of boundary layer? delta=5*(LHORI)/sqrt(Re(L)).

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