I have generated a NACA 4412 profile of which the polynomial equation is corrected to attain a sharp trailing edge. While importing in Construct2D, it detects a blunt edge. Airfoil profile link attached. Any help is appreciated.
https://copy.com/infopIpnKLbc
hi Rajib Roy.....Can you please tell me how do you give boundary conditions to your mesh...I tried to use this mesh in openfoam...
Thanks for your help...
Hello Rejish, Sample boundary conditions could be found at tutorial/incompressible/simpleFoam/aifoil2D
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I have generated a NACA 4412 profile of which the polynomial equation is corrected to attain a sharp trailing edge. While importing in Construct2D, it detects a blunt edge. Airfoil profile link attached. Any help is appreciated.
https://copy.com/infopIpnKLbc
Last edit: Rajib Roy 2014-03-26
hi Rajib Roy.....Can you please tell me how do you give boundary conditions to your mesh...I tried to use this mesh in openfoam...
Thanks for your help...
Hello Rejish,
Sample boundary conditions could be found at tutorial/incompressible/simpleFoam/aifoil2D