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kabilan August 16, 2011 11:33

reynolds no
 
hai forum
i have airfoil model,velocity,density and viscosity.
rey.no=rho*vel*x/viscosity...
how can i calculate the reynolds number, i don't know howmuch should i substitute for x value. thanks

husker August 16, 2011 12:20

Hi,

x is the characteristic length. Here, it is the chord of your airfoil.

Re = Rho * Vel * c / Mhu


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