Guide for authors

正Each of the sections below provides essential information for authors.We recommend that you take the time to read them before submitting a contribution to Acta Mechanica Sinica.We hope our guide to authors may help you navigate to the appropriate section.How to prepare a submission This document provides an outline of the editorial process involved in publishing a scientific paper in Acta Mechanica Sinica.     

Guide for authors

Each of the sections below provides essential information for authors. We recommend that you take the time to read them before submitting a contribution to Acta Mechanica Sinica. We hope our guide to authors may help you navigate to the appropriate section.     

Guide for authors

Each of the sections below provides essential information for authors. We recommend that you take the time to read them before submitting a contribution to Acta Mechanica Sinica. We hope our guide to authors may help you navigate to the appropriate section.     

Guide for authors

正Each of the sections below provides essential information for authors.We recommend that you take the time to read them before submitting a contribution to Acta Mechanica Sinica.We hope our guide to authors may help you navigate to the appropriate section.How to prepare a submission This document provides an outline of the editorial process involved in publishing a scientific paper in Acta Mechanica Sinica.     

Guide for authors

<正>Each of the sections below provides essential information for authors.We recommend that you take the time to read them before submitting a contribution to Acta Mechanica Sinica.We hope our guide to authors may help you navigate to the appropriate section.How to prepare a submission This document provides an outline of the editorial process involved in publishing a scientific paper in Acta Mechanica Sinica.●Five parts should be included in your submission,which are full paper(full text,figures,tables and supplementary information),highlight,cover letter,copyright transfer statement(CTS)and a     

变截面欧拉梁自由振动分析的重采样微分求积法

采用重采样微分求积法求解了变截面欧拉梁的自由振动问题。推导了变截面梁的控制方程离散格式,采用重采样矩阵方法对边界条件进行处理,给出了变截面梁自由振动算法。采用本文方法对不同类型截面形式和不同边界条件的变截面梁进行自由振动分析,并和其他解法进行比较。计算结果表明,本文方法可以适用于不同变截面类型和不同边界条件,计算精度与解析解吻合良好,具有良好的收敛性能。在同等精度条件下网格点数少于现有计算方法。重采样转换矩阵边界处理方法相比于传统边界处理方法具有更快的收敛性能。     

变截面电磁波导的辛分析

电磁波导的求解可将基本方程导向Hamilton体系、辛几何的形式。横向的电场和磁场构成了对偶向量。辛体系便于处理不同介质波导的界面连接条件。正则对偶方程、分离变量法、Hamilton算子矩阵本征值问题、共轭辛正交归一关系、本征解的展开定理等整套理论,可以适用于多种波导的课题,有利于不同截面的波导连接、以及与共振腔的连接等。本文分析了两段不同材料不同截面对接的平面波导作为例题,表明辛体系用于波导的分析是有力的。     

惯性／DGPS精密进场着陆引导系统

为确保飞机精确直线飞越预定点上空并具备精密进场着陆引导能力 ,研制了机载惯性 /DGPS精密进场着陆引导系统。该系统通过综合技术将惯性导航系统与差分 GPS有效组合 ,不仅定位精度高、工作可靠 ,而且输出信息实时、连续 ;通过着陆引导轨迹及引导画面的精心设计 ,为飞行员提供图形化的、精确安全的进场着陆引导信息 ,引导飞机至决断高处 ,从而解决了飞机全天候尤其是在复杂气象条件的进场着陆引导问题。本文介绍了该系统的方案、组成、系统特点、技术难点以及试飞结果。试飞中飞行员反映该系统精度高 ,引导画面图形直观 ,操作简便 ,能满足复杂气象条件下的进场着陆引导要求     

汽车变速箱Hy-Vo齿形链磨损特性的研究

针对汽车变速箱传动系统高转速、强磨损的特殊要求,通过内-外复合啮合Hy-Vo齿形链300 h的高速磨损台架试验,研究了汽车变速箱链条的摩擦磨损特性,对啮合传动过程中链条铰链副以及链板外廓与链轮的接触区进行了局部微观磨损形貌分析.结果表明:汽车变速箱Hy-Vo齿形链的综合磨损伸长由对滚异型销轴磨损以及链板外廓磨损组成,其中,对滚异型销轴的磨损机制为疲劳磨损.     

通气超空泡形态控制方法的数值模拟

根据Logvinovich独立膨胀原理发展了一种用于非定常通气超空泡形态的计算方法,并运用该方法对通气超空泡形态控制进行了数值仿真.研究表明:调整流场压力、模型速度、空化器阻力系数对超空泡长度的控制范围较大,响应速度较快;调整通气量对超空泡长度控制范围较小,响应速度较慢;此外改变超空泡内部模型的尺度和结构也可以对通气超空泡形态进行控制.     

Nonlinear Normal Modes and Their Bifurcations for an Inertially Coupled Nonlinear Conservative System

This work concerns the nonlinear normal modes (NNMs) of a 2 degree-of-freedom autonomous conservative spring–mass–pendulum system, a system that exhibits inertial coupling between the two generalized coordinates and quadratic (even) nonlinearities. Several general methods introduced in the literature to calculate the NNMs of conservative systems are reviewed, and then applied to the spring–mass–pendulum system. These include the invariant manifold method, the multiple scales method, the asymptotic perturbation method and the method of harmonic balance. Then, an efficient numerical methodology is developed to calculate the exact NNMs, and this method is further used to analyze and follow the bifurcations of the NNMs as a function of linear frequency ratio p and total energy h. The bifurcations in NNMs, when near 1:2 and 1:1 resonances arise in the two linear modes, is investigated by perturbation techniques and the results are compared with those predicted by the exact numerical solutions. By using the method of multiple time scales (MTS), not only the bifurcation diagrams but also the low energy global dynamics of the system is obtained. The numerical method gives reliable results for the high-energy case. These bifurcation analyses provide a significant glimpse into the complex dynamics of the system. It is shown that when the total energy is sufficiently high, varying p, the ratio of the spring and the pendulum linear frequencies, results in the system undergoing an order–chaos–order sequence. This phenomenon is also presented and discussed.     

An integration method for detecting chaotic responses of nonlinear systems subjected to double excitations

A methodology designed for identifying chaos of the nonlinear systems subjected to double excitations is proposed. Based on simulations in this study, it is shown by bifurcation diagram that method of Poincaré sections, the conventional chaos-observing method, fails to pinpoint the onset of chaotic motions with the nonlinear systems subjected to double excitations. To remedy this problem, “K_s integration method” is proposed, which integrates the distance between trajectories and origin in phase plane over an excitation period and designates the obtained integration values as K_s's to take the roles of the sampling points derived by Poincaré sections in constructing bifurcation diagram. This “K_s integration method” is shown capable of providing valuable information in bifurcation diagram such that the parameter range leading to chaos can be easily decided and the number of distinguishable time-domain responses can be determined.