PROBLEM: At the instant shown, the 12-in. crank on the small aircraft landing gear actuation in Figure P7.41 rotates counterclockwise at 18 rpm and decelerates at 3.5 rad/s². Use the relative acceleration method to graphically and analytically determine the angular velocity and angular acceleration of the wheel assembly.
321
5
30'
26"
30"
FIGURE P7.41