How to design a propeller to analyse it by CFD in Ansys
Hi. I got a graduate project on Quadrotors. Shortly, i need its aerodynamic characteristics and so i will analyse its propeller alone, other rigid bodies are not included. Ansys has "BladeGen" in it which allows to model numberr of different propellers, fans, turbomachinery parts. Can anyone help me how to use BladeGen, hot to model a normal axial two bladed propeller with it?