1 Reply Latest reply on Feb 27, 2009 10:52 PM by reeshi pradhan

    Lift Coefficient

    reeshi pradhan
      Which equation is to be used to find Lift Coeff. of airfoil in Floworks?
      This is equation I had used.
      But result vary.

      {GG Y - Component of Force 1}/(Re*Dynamic viscosity)^2* span length of airfoil)*(2*density of air*Cord length)

      Velocity in term of reynold's no.