A load of 100 Ib at the wing tip of a fighter plane produced a corresponding deflection of 0.78 in.
If the fundamental bending frequency of the same wing is 622 cpm, approximate the new bending frequency when a 320-lb fuel tank (including fuel) is attached to the wing tip.
The response must be typed, single spaced, must be in times new roman font (size 12) and must follow the APA format.