coutinho82
New member
- Jul 3, 2015
- 1
H Everyone!
I'm calculating the bending stiffness for a helicoper blade part, which links the blade to the the cube. That fitting was modeling by Femap. Next, a unitary force was applied at the tip of the blade in order to obtained the node rotation
where the bending stiffness (N/m) want to be calculate (euler theory). So, how this procedure should be done take into account the blade rotation (492 RPM) with the centrifugal force?
thanks
I'm calculating the bending stiffness for a helicoper blade part, which links the blade to the the cube. That fitting was modeling by Femap. Next, a unitary force was applied at the tip of the blade in order to obtained the node rotation
where the bending stiffness (N/m) want to be calculate (euler theory). So, how this procedure should be done take into account the blade rotation (492 RPM) with the centrifugal force?thanks