Consider the aircraft engine and mount indicated in the figure below. Model the

Question

Consider the aircraft engine and mount indicated in the figure below. Model the engine as a fixed mass at the end of a massless beam. Assume the stiffness of the mount can be approximated by the 3. stiffiness nclationeship for ape anilrbam, k EI 3pp k birdl flying towards t aircraft at 50 mph strikes the engine while the aircraft is going 150 mph. Calculate the response and estimate maximum deflection for the case of an aluminum mount 1.5 m long with m 1000 kg,s0.01, E- 6.9x 1010 N/m 2, and 1-0.3 ? m. Wing, ground massless Mount, k keff x(t) FoU) Engine, m

Explanation / Answer

The answer of the following question are as follows.

I got this value by solving the question..

The maximum deflection=.025m

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