CFD Online Discussion Forums

CFD Online Discussion Forums (
-   Main CFD Forum (
-   -   reynolds no (

kabilan August 16, 2011 11:33

reynolds no
hai forum
i have airfoil model,velocity,density and viscosity.*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


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

Re = Rho * Vel * c / Mhu

All times are GMT -4. The time now is 00:18.