Hi All,
I am currently designing a drone frame, and performing FEA on a quarter model (see below).
The arm has a 10N load acting upwards at the end, while the top surface of the main body is fixed. This is to simulate the forces occurring when the drone accelerates upwards at maximum...
Hi, please see the attached drawing. I've set up an FEA for a part (a rocker for a monoshcok suspension system) and constrained the rod as described in the photo. Please can someone explain to me why the part is able to complete an FEA analysis rather than spinning around indefinitely? Many thanks