Learning Forum

[Seyi Oluwadare]

Please, how do I compute aerodynamics force over a section part of a blade which was cut out with iso-clip in order to get the normal force and tangetial force , that to decompose the force in x, y, z direction in other to get the aerodynamic force.

 

I have been trying to do that in Fluent but not getting how to do it... My first try is to integrate static pressure and wall shear stress over the surface. I could get the x ,y,z componets of viscouse force but I could get that of pressure force after the integration of static pressure. 

[Essence]

Hello,

Could you please share the screenshot of how you found out the X, Y and Z components of viscous force over the iso-clip?