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The runway surface of an aircraft is described as z(t) = Z, cost and the landing gear of the airplane is roughly modeled as a mass-spring-damper system. Assume m = 2500 kg, = 60 rad/sec, and k=8×106 N/m. Determine, (a) an expression for the transmission ratio, TR in terms of 5 and plot TR vs. 5, (b) the value of such that the maximum (TR)max = 0.4. 22 (2) z(t) m z(t)= to cost Runway
Please do not copy already posted answers.
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