An aircraft landing gear can be idealized as a single degree of freedom spring-mass-damper system. The desirable damping characteristics of such a system is:
(A) Under damped
(B) Over damped
(C) Critically damped
(D) Undamped
An aircraft landing gear can be idealized as a single degree of freedom spring-mass-damper system. The desirable damping characteristics of such a system is:
(A) Under damped
(B) Over damped
(C) Critically damped
(D) Undamped