1.Unlike the existing literature that the absorber was considered as a spring-damper-mass system and the inertia effect of the spring was neglected, the last effect was taken into consideration in this paper.
2.On the basis of reference (superscript [6]), the influence of damping of shimmy damper, moment of inertia of wheel, tire cornering stiffness and strut tilt stiffness on parametric shimmy stability of aircraft wheel is investigated in the paper.
