Bharathsf
Aerospace
- Feb 5, 2012
- 35
I have a flange on which a motor weighing 175 kgs is mounted. The CG of the motor is 155 mm from the flange. The flange is fitted to a shell using 12 bolts circumferentially. What would be the load on each of the boltts due to the eccentric load of the motor. The load is perpendicular to the axis of the bolt. I know there is going to be a moment and a vertical shear load. What would be the secondary shear due to the moment and which bolts would be in tension and which would be in compression?