钢丝绳检测数据的可靠性评定方法

该系统对钢丝绳试验站检验数据及日数据微机处理。通过原始数据的录入，可以自动生成成试验站用各种报表、判断是否符合《煤矿安全规程》并进行可靠性评定。     

Numerical simulation of helicopter maneuverability in aerobatics research

A method for calculating available overloads and for subsequent evaluation of helicopter maneuverability is proposed taking into account specific operational conditions.     

Don Pettit 国际空间站微重力流体实验与若干现象的解析

Don Pettit 是美国NASA 的资深宇航员, 2002 年11 月至2003 年5 月, 在国际空间站工作期间, 进行了一系列名为Saturday Morning Science的微重力实验. Don Pettit 实验揭示了微重力下一些令人惊奇的现象, 涉及流体力学、气泡动力学、晶体生长以及运动学的诸多基础问题, 是能够获得的国际空间站为数不多的微重力实验资料, 具有重要研究意义. 实验包括14 组流体实验和7 组力学实验, 而流体实验又大致分为水膜实验和水球实验, 包括大尺寸水膜制备、扩散和对流、Marangoni 对流、薄膜结晶、水球/气泡旋转等. 本文对Don Pettit 实验的流体部分进行了介绍, 并对其中的Marangoni对流和薄膜结晶实验现象进行了解析.      

On the effects of each term of the geopotential perturbation along the time I: Quasi-circular orbits

This paper provides a useful new method to determine minimum and maximum range of values for the degree and order of the geopotential coefficients required for simulations of orbits of satellites around the Earth. The method consists in a time integration of the perturbing acceleration coming from each harmonic of the geopotential during a time interval T. More precisely, this integral represents the total velocity contribution of a specific harmonic during the period T  . Therefore, for a pre-fixed minimum contribution, for instance 1×10^-8$1\times {10}^{-8}$ m/s during the period of time T, any harmonic whose contribution is below this value can, safely, be neglected. This fact includes some constraints in the degree and order of the terms which are present in the geopotential formula, saving computational efforts compared to the integration of the full model. The advantage of this method is the consideration of other perturbations in the dynamics (we consider the perturbations of the Sun, the Moon, and the direct solar radiation pressure with eclipses), since these forces affect the value of the perturbation of the geopotential, because these perturbations depend on the trajectory of the spacecraft, that is dependent on the dynamical model used. In this paper, we work with quasi-circular orbits and we present several simulations showing the bounds for the maximum degree and order (M) that should be used in the geopotential for different situations, e. g., for a satellite near 500 km of altitude (like the GRACE satellites at the beginning of their mission) we found 35?M?198$35?M?198$ for T=1$T=1$ day. We analyzed the individual contribution of the second order harmonic (_J2$J_2$) and we use its behavior as a parameter to determine the lower limit of the number of terms of the geopotential model. In order to test the accuracy of our truncated model, we calculate the mean squared error between this truncated model and the “full” model, using the CBERS (China-Brazil Earth Resources Satellite) satellite in this test.     

月面巡视器实时动力学建模与牵引控制

为实现月面巡视器GNC系统的闭环测试,研究了六轮摇臂式巡视器在月表崎岖地形、松软土壤和低重力环境下的动力学建模与控制问题。基于弹塑性轮—土力学和粘弹性运动副约束分析,建立了巡视器的牛顿—欧拉动力学模型。以跟踪期望速度、角速度为目标,采用速度协调控制和车轮滑移控制,完成了巡视器闭环牵引控制。在实时操作系统下实现了巡视器动力学模型和牵引控制系统,并建立了三维可视化平台,对该动力学模型和牵引控制方法进行验证。测试结果证实了建立的动力学模型准确、稳定,可以真实地模拟巡视器在月球表面的运动行为和轮—土作用关系,且满足运动副的约束;所设计的牵引控制方法可以较准确地实现巡视器跟踪期望的运动。     

复合推进剂线粘弹本构方程的细观力学分析(Ⅱ)非球颗粒增强效应分析

应用等效夹杂的细观力学理论,针对一种与取向相关的细长椭球颗粒填充情况,研究复合固体推进剂粘弹本构方程。发现颗粒对基体的增强效应主要体现在颗粒的纵向,得到了颗粒无序取向对基体的增强效应与颗粒单轴取向对基体沿该取向的增强效应之间存在一个定量的等效关系。     

粉末冶金坯体成形过程中产生裂纹预测的一种算法

介绍了金属粉末成形中裂纹的种类与成因,从理论和应用上详细论述了基于细观处理的损伤力学方法在金属粉末成形中裂纹预测中的应用,分析了这种方法的优缺点并提出了指导性意见.     

钢筋混凝土受弯构件矩形截面的三阶段刚度公式推导

我国钢筋混凝土结构设计规范中,钢筋混凝土受弯构件的刚度公式是在半理论半实验的基础上建立起来的.本文运用混凝土力学的方法来推导钢筋受弯构件在不同阶段的刚度公式.     

含多裂纹结构的概率损伤容限评定方法

将概率断裂力学理论与损伤容限／耐久性设计方法有机地结合起来,考虑结构初始疲劳裂纹尺寸及其扩展过程的随机性,建立了裂纹相互独立条件下的多裂纹结构的全寿命概率损伤容限评定模型,并成功地运用于机翼主梁的可靠性评定,给出指定疲劳寿命下的安全可靠度或指定安全可靠度下的安全疲劳寿命。     

疲劳寿命分布模型及其拟合优度检验

从细观损伤力学的角度出发,建立了几种常用寿命分布所对应的物理模型,给出了相应分布中参数矢量的似然估计表达式,并采用先进拟合优度检验方法对母体分布进行了假设检验。在假定母体服从正态分布、对数正态分布或Ｗｅｉｂｕｌ分布的条件下,计算了相应疲劳寿命的Ｂ基值。