Effect of damping on impact response of a two degrees of freedom system
暂无分享,去创建一个
Abstract The impact response of a system consisting of a main mass on which a critical element of much smaller mass is mounted, is analyzed. Equations of motion are non-dimensionalized and a closed form solution obtained. System parameters are the two damping ratios and the frequency ratio. Maximum values of the non-dimensional acceleration of the critical element and the product of its acceleration and displacement are computed. Results are presented in a form to permit optimum design of the system.
[1] Raymond D. Mindlin. Dynamics of package cushioning , 1945 .
[2] C. Crede. Vibration and shock isolation , 1951 .
[3] M. Hundal. Optimum damping for impact absorbers , 1977 .