fulcrum
Jul3-04, 01:52 PM
Hi folks,
I did try a lot of analysis on aerofoils using FLOTRAN from some time back. I have managed to do flow path traces and velocity vectors and stuff using FLOTRAN. So I have managed to visualize flow, if you will. What I need to understand is how to calculate (using FLOTRAN itself) the lift and drag forces on the foil Ive analysed. Or atleast the coefficients. Could anyone help me out?
Im using ANSYS 5.4...thanks for any help.
--Fulcrum
I did try a lot of analysis on aerofoils using FLOTRAN from some time back. I have managed to do flow path traces and velocity vectors and stuff using FLOTRAN. So I have managed to visualize flow, if you will. What I need to understand is how to calculate (using FLOTRAN itself) the lift and drag forces on the foil Ive analysed. Or atleast the coefficients. Could anyone help me out?
Im using ANSYS 5.4...thanks for any help.
--Fulcrum