The gear dynamics analysis is, according to the theory of vibrate dynamics, to study the basic rule of vibration, shock and noise which created by gear system while transferring power and motion.
齿轮动力学分析是利用振动力学理论，研究齿轮系统在传递动力和运动过程中振动、冲击、噪声的基本规律，对齿轮传动的降噪、降振非常重要。
The shock compression of condensed matter can be effectively dealt with by molecular dynamics, and has been applied to many fields of science.
用分子动力学方法可以有效地研究凝聚介质的激波压缩，并在许多领域得到了广泛应用。
The paper considers home shock absorber and vehicle as object to have a study on nonlinear characteristic of shock absorber in vehicle passive suspension and vehicle ride dynamics.
本文以国产减振器与汽车为研究对象，目的是对汽车被动悬架中减振器非线性特性及包含这种非线性特性的汽车乘座动力学进行深入研究。
The dynamic nonlinear viscoelastic model and dropping shock model of multilayer fruit were developed in terms of the dynamics characteristics obtained by dropping shock tests.
基于损伤条件下果实刚性跌落冲击变形特征，提出一表征其非线性黏弹性的动态流变模型，建立多层果实跌落冲击模型。
The result will give a basis for free design of shock absorber and vehicle ride dynamics system and lay solid foundation for investigation of suspension controlling and ground damage systematically.
本文研究结果可为减振器及汽车乘座动力学系统自主设计提供依据，也可为可控悬架及路面损坏问题的研究奠定基础。
The reasons of forming a shock-cell structure and changing the flow field pressure were analyzed with jet dynamics.
根据射流动力学理论，分析了产生这种波系结构和流场压力变化的原因。
Based on the dynamics of structure, this paper presented apratical method of two steps by double model for calculating the complexity shock-isolating system with nonlinear stiffness.
基于结构动力学理论，提出了一种用于分析计算复杂非线性隔冲减振系统的双模型两步计算法。
We study the dynamics of oil consumption and oil price in a situation where the pending oil shock and strategic oil reserve plan are relevant.
本文采用动态最优控制方法分析了在面临外生性石油供给冲击时，国家石油战略储备计划对国内石油消费以及石油价格走势的动态影响。
Experimental techniques based on the dynamics of shock wave attenuation were used to produce decaying triangular shock pulse in LY12 Al samples of plate-impact spall tests.
就样品中呈现三角形脉冲的平板冲击实验而言，样品中可以存在一些高拉伸应力区域并发生多次层裂。
When the Angle of attack is small or more than Angle of attack of buffeting, the shock control bump has little effect on the dynamics of airfoil.
而当迎角较小或超过抖振迎角后该激波控制鼓包不会对基本翼型的气动性能产生较大影响。
When the Angle of attack is small or when it is larger than the buffet onset Angle, the shock control bump has little effect on the dynamics of the airfoil.
而当迎角较小或超过抖振迎角后该激波控制鼓包不会对基本翼型的气动性能产生较大影响。
When the Angle of attack is small or when it is larger than the buffet onset Angle, the shock control bump has little effect on the dynamics of the airfoil.
而当迎角较小或超过抖振迎角后该激波控制鼓包不会对基本翼型的气动性能产生较大影响。
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