scholarly journals Methods for Atomistic Simulations of Linear and Nonlinear Damping in Nanomechanical Resonators

2015 ◽  
Vol 24 (5) ◽  
pp. 1462-1470 ◽  
Author(s):  
Zahra Nourmohammadi ◽  
Sankha Mukherjee ◽  
Surabhi Joshi ◽  
Jun Song ◽  
Srikar Vengallatore
Nano Letters ◽  
2021 ◽  
Author(s):  
Shelender Kumar ◽  
Shishram Rebari ◽  
Satyendra Prakash Pal ◽  
Shyam Sundar Yadav ◽  
Abhishek Kumar ◽  
...  

2020 ◽  
pp. 13-22
Author(s):  
Ze-Qi Lu ◽  
Dong-Hao Gu ◽  
Ye-Wei Zhang ◽  
Hu Ding ◽  
Walter Lacarbonara ◽  
...  

1974 ◽  
Vol 96 (1) ◽  
pp. 51-59 ◽  
Author(s):  
S. M. Wang

The dynamic torsional analysis of gear train systems has implemented many practical system designs. A computer analysis to predict the steady-state torsional response of a gear train system is presented in reference [1]. The current paper extends this work to the linear and nonlinear transient analysis of complex torsional gear train systems. Factors considered in the formulation are time-varying gear tooth stiffness, gear web rigidity, gear tooth backlash, shafts of nonuniform cross section, linear and nonlinear damping elements, multishock loadings, and complex-geared branched systems. For linear systems, the equations of transient motion are derived and closed-form solutions can be obtained by the state transition method [2]. For nonlinear systems, numerical methods are also presented. The method may be used as a means to analyze gear train start/stop operational problems, as well as constant speed response subject to internal and external disturbances.


2021 ◽  
Vol 126 (17) ◽  
Author(s):  
Letizia Catalini ◽  
Massimiliano Rossi ◽  
Eric C. Langman ◽  
Albert Schliesser

2006 ◽  
Vol 129 (1) ◽  
pp. 32-38
Author(s):  
Yves Gourinat ◽  
Victorien Belloeil

An adaptive approach of vibrating thin structures is proposed here. The method consists in applying an equivalent adimensional damping ratio to each potential resonance. This ratio is deduced from experimental data obtained in vacuum facility, in relation with frequencies, for several structural technologies. Consequently, it is possible to calculate the structure in a linear nondissipative context, valid out of resonance bands, and truncated in those bands. Thus, the equivalent damping ratio is directly used to define adimensional resonance truncation bandwith and level. The contribution consists in tested and applied modal methodology and algebraic representations of damping including several dissipations—viscous and internal microfrictions—inducing a nonmonotonous model. The here aim is to provide realistic recommendations for simple vibrational analysis of aerospace thin structures—panels and stiffeners.


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