3.44 The landing gear of an airplane can be idealized as the spring-mass-damper system shown in Fig. 3.52 [3.16]. If the runway surface is described y(t) = y cos wt, determine the values of k and c that limit the amplitude of vibration of the airplane (x) to 0.1 m. Assume m = 2000 kg, yo = 0.2 m, and @ = 157.08 rad/s. pos y(t) x(t) H m (b) Wheel Runway Housing with strut and viscous damping Mass of aircraft, m to

3.44 The landing gear of an airplane can be idealized as the spring-mass-damper system shown in Fig. 3.52 [3.16]. If the runway surface is described y(t) = y cos wt, determine the values of k and c that limit the amplitude of vibration of the airplane (x) to 0.1 m. Assume m = 2000 kg, yo = 0.2 m, and @ = 157.08 rad/s. pos y(t) x(t) H m (b) Wheel Runway Housing with strut and viscous damping Mass of aircraft, m to

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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