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 |
Hi,
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 12:37. |