复合材料层合梁的屈曲

本文在铁摩辛柯梁理论基础上,利用迭合刚度方法及Hamilton原理建立了层合梁屈曲问题控制方程,并用此控制方程求解了在具体边界条件下层合梁的屈曲问题,得出了无论在什么边界条件下层合梁的最小屈曲载荷不会大于等效剪切刚度系数C的结论.     

复合材料层合圆柱壳的有限元分析

本文根据Reissner-Mindlin型的全局位移场(一阶和三阶)，应用有限元预测一修正法，数值计算和分析了机械载荷作用下复合材料层合圆柱壳的挠度和横向剪应力。首先按照一般的有限元分析过程(没有引入剪切修正系数)计算出层合圆柱壳的挠度预测值；然后利用Lagrange插值构造横向剪应力的一般形式，使得满足层间连续和表面上为零的条件，通过最小二乘法拟合三维应力平衡方程获得横向剪应力；最后在单元上计算和引入剪切修正系数，再经过有限元分析计算出层合圆柱壳的挠度修正值。数值计算结果与三维线弹性解的比较表明，挠度修正值和横向剪应力的精度是十分满意的。     

复合材料层合壳有限元分析的预测-修正法

对于复合材料层合壳的有限元分析，本文根据Reissner-Mindlin型的全局位移场给出了一个预测一修正法。首先按照一般的有限元分析过程(没有引入剪切修正系数)计算出全局响应(如挠度，频率和屈曲载荷等)的预测值；然后利用Lagrange插值构造横向剪应力的一般形式，使得满足层间连续和表面上为零的条件，通过最小二乘法拟合三维应力平衡方程获得横向剪应力；最后在单元上计算和引入剪切修正系数，再经过有限元分析计算出全局响应的修正值。     

国产润滑油的压粘系数和固化压力

润滑油的压粘系数和固化压力是弹流理论应用于摩擦学工程设计的关键试验数据。本文报道了20种国产润滑油的压粘系数和其中16种润滑油的最小固化压力的测定结果,并对不同油田的基础润滑油、不同化学结构的合成润滑油和不同用途的工业润滑油的压粘系数和固化压力进行了分析比较。     

受分布载荷复合材料层合梁应力分析的一般理论

为了克服层合梁经典理论的缺点，提高层间应力的计算精度，提出了受分布载荷层合梁应力分析的一般理论。首先根据叠加原理将原始受力状态分解成对称与反对称受力状态。然后用正交完备的三角级数和勒让德级数构造这两种受力状态中每一铺层与层间胶层的位移场，并应用广义势能原理确定位移场中的待定系数，从而确定层合梁的位移场和应力场。同时，单层梁与单层梁之间的胶层被视为各向同性材料并且与其它材料层具有相似的力学特性，即具有有限厚度、有限弹性常数。计算结果显示,这种解法的收敛性非常好，根据物理方程与根据平衡方程得到的横向剪应力和正应力分布非常一致。     

基于回传波射矩阵法的复合材料层合框架振动特性分析

将求解弹性杆系结构动态响应的回传波射矩阵法应用于层合框架的固有频率和模态的求解.用回传波射矩阵法得到单位脉冲载荷作用下层合框架的频响函数,然后由频响函数曲线的波峰确定层合框架结构的固有频率.最后通过回传波射矩阵法控制方程系数矩阵的伴随矩阵得到结构的振动模态.将对称铺层简支梁计算结果与用经典理论算得的解析解进行比较,验证了回传波射矩阵法计算结果具有很高的精度.然后对9根杆组成的平面层合框架进行计算,表明回传波射矩阵法可以有效地计算层合框架结构的固有频率和模态.     

压电层合梁静动力学分析的高精度梁单元

给出了一个对复合材料压电层合梁进行数值分析的高精度压电层合梁单元。基于Shi三阶剪切变形板理论的位移场和Layer-wise理论的电势场,用力-电耦合的变分原理及Hamilton原理推导了压电层合梁单元列式。采用拟协调元方法推导了一个可显式给出单元刚度矩阵的两节点压电层合梁单元,并应用于压电层合梁的力-电耦合弯曲和自由振动分析。计算结果表明,该梁单元给出的梁挠度和固有频率与解析解吻合良好,并优于其它梁单元的计算结果,说明了本文所给压电层合梁单元的可靠性和准确性。研究结果可为力-电耦合作用下压电层合梁的力学分析提供一个简单、精确且高效的压电层合梁单元。     

黏弹性层合圆柱壳的临界轴压分析

基于经典屈曲理论，研究了轴向受压黏弹性复合材料层合圆柱壳的临界屈曲载荷. 利用Boltzmann线性积分型本构关系描述铺设单层的各向异性黏弹性行为. 结合解析与数值 方法，由Donnell型屈曲控制方程以及边界条件的Laplace变换导出相空间的特征方程，根 据Laplace逆变换的极值定理，获得层合圆柱壳的瞬时弹性临界载荷与持久临界载荷. 针对 多组铺设方式，通过数值算例重点分析了临界载荷随铺设角的变化特征，两种临界载荷的峰 值点差异程度与铺设方式、几何参数以及材料类型的关系，得到了一些对黏弹性层合圆柱壳 的优化设计有参考价值的结论.     

SMA纤维混杂层合梁的材料阻尼

研究一类由形状记忆合金（SMA）和普通纤维混杂而成的层合梁的阻尼特性,基于最大应变能理论提出SAM混杂层合梁的等效材料阻尼预测的数学模型,其中,单层材料的弹性性能和阻尼性能分别采用多胞模型及其阻尼细观力学分析模型确定,利用正交各向异性层合梁的铁木辛柯理论分析梁的变形,通过数值算例分析了SMA含量,纤维铺设角对梁的等效阻尼比的影响。     

压电/压磁层合纳米梁屈曲及自由振动的研究

针对压电/压磁层合纳米梁屈曲、自由振动问题,基于非局部理论与正弦剪切型变形梁理论,建立了力学模型;利用哈密顿原理推导出层合梁运动方程与边界条件;通过数值解法求得层合梁临界屈曲载荷与自由振动频率。对数值结果分析可知:磁电弹夹层对压电/压磁层合纳米梁屈曲和自由振动的影响不能忽略;磁电弹夹层中压电或压磁材料的体积分数和夹层厚度为主要影响因素;分析得到的影响规律可为此类材料在工程中的应用提供理论参考。     

Diffusion baroeffect in a capillary in a broad range of knudsen numbers

The magnitude of the diffusion baroeffect in a capillary is calculated in the entire range of Knudsen numbers based on a solution of BGK equations for a binary gas equation. The theoretical magnitudes of the baroeffect agree well with the experimental results obtained in a broad range of Knudsen numbers. The thermodynamic coefficients are calculated, and the Onsager reciprocal relation is demonstrated, from which in the limit of a viscous system it follows that the barodiffusion constant is equal to the coefficient of diffusion slippage.Translated from Zhurnal Prikladnoi Mekhaniki i Tekhnicheskoi Fiziki, No. 2, pp. 74–79, March–April, 1973.     

一类带柔性附件充液航天器姿态机动控制

基于Lyapunov稳定性理论研究了用动量轮控制一类带轻质悬臂梁附件的充液航天器的姿态机动控制问题, 其中晃动液体用黏性力矩球摆模型代替, 悬臂梁附件用若干集中质量代替. 用动量矩定理和Lagrange方程分别推导得到航天器主刚体、等效球摆、等效集中质量的动力学方程, 所用反馈控制律包含了与动量轮角加速度密切相关的权重因子, 利用系统初、终状态和到达最终姿态所需时间解析确定此权重因子. 同时利用Lyapunov稳定性理论得到了实现最终姿态机动的稳定性判据. 数值仿真表明所用控制律的有效性, 分析附件的相对主刚体平面的转角、相对系统质心的高度、长度、刚度、质量、阻尼系数和到达最终姿态所需时间等因素对控制过程中航天器剩余章动角的影响大小.      

Effects of characteristic material lengths on mode III crack propagation in couple stress elastic–plastic materials

The asymptotic fields near the tip of a crack steadily propagating in a ductile material under Mode III loading conditions are investigated by adopting an incremental version of the indeterminate theory of couple stress plasticity displaying linear and isotropic strain hardening. The adopted constitutive model is able to account for the microstructure of the material by incorporating two distinct material characteristic lengths. It can also capture the strong size effects arising at small scales, which results from the underlying microstructures. According to the asymptotic crack tip fields for a stationary crack provided by the indeterminate theory of couple stress elasticity, the effects of microstructure mainly consist in a switch in the sign of tractions and displacement and in a substantial increase in the singularity of tractions ahead of the crack-tip, with respect to the classical solution of LEFM and EPFM. The increase in the stress singularity also occurs for small values of the strain hardening coefficient and is essentially due to the skew-symmetric stress field, since the symmetric stress field turns out to be non-singular. Moreover, the obtained results show that the ratio η introduced by Koiter has a limited effect on the strength of the stress singularity. However, it displays a strong influence on the angular distribution of the asymptotic crack tip fields.     

船用气水分离器惯性级流场分析及阻力特性研究

采用二阶全展开ETG有限元与大涡模拟（LES）相结合的算法，对120－20－35－3型船用气水分离器惯性级在不同雷诺数条下的流动进行了模拟，通过其中一组雷诺数条件下计算所得该实验件阻力系数与物理实验所得阻力系数相比较，确定出该雷诺数条件下采用大涡模拟时所需的亚格子应力模型常数，将该常数带入其它各组雷诺数条件下的计算中，并将计算结果与相同条件下的物理实验结果相比较，证实了该常数的通用性。该常数一经确定，对各雷诺数条件下的流场进行分析，结果反映出采用二阶全展开ETG有限元与大涡模拟（LES）相结合的算法可以捕捉到非常丰富的涡系及涡动的时变过程。在流场分析的基础上本文计算了该实验件内的能耗场，计算结果表明实验件内的能耗主要集中在大涡丰富的区段内。     

A dynamic global-coefficient mixed subgrid-scale model for large-eddy simulation of turbulent flows

A dynamic global-coefficient mixed subgrid-scale eddy-viscosity model for large-eddy simulation of turbulent flows in complex geometries is developed. In the present model, the subgrid-scale stress is decomposed into the modified Leonard stress, cross stress, and subgrid-scale Reynolds stress. The modified Leonard stress is explicitly computed assuming a scale similarity, while the cross stress and the subgrid-scale Reynolds stress are modeled using the global-coefficient eddy-viscosity model. The model coefficient is determined by a dynamic procedure based on the global-equilibrium between the subgrid-scale dissipation and the viscous dissipation. The new model relieves some of the difficulties associated with an eddy-viscosity closure, such as the nonalignment of the principal axes of the subgrid-scale stress tensor and the strain rate tensor and the anisotropy of turbulent flow fields, while, like other dynamic global-coefficient models, it does not require averaging or clipping of the model coefficient for numerical stabilization. The combination of the global-coefficient eddy-viscosity model and a scale-similarity model is demonstrated to produce improved predictions in a number of turbulent flow simulations.     

Shape sensitivity analysis for non-differentiable performance measures in multiscale crack propagation simulation using regression hybrid method

In this paper, we present a regression hybrid method that calculates shape sensitivity coe?cients for multiscale crack propagation problems with performance measures that are non-differentiable in numerical implementation. These measures are crack propagation speed (or crack speed) defined at atomistic level obtained by solving coupled atomistic/continuum structures using the bridging scale method (BSM). The major contributions of this paper are: first, by analyzing the characteristics of the performance measures of crack speed in design space, this paper verifies for the first time that these measures are theoretically continuous and differentiable with respect to design variables, and as a result, the sensitivity coe?cients exist in theory; second, to overcome the non-differentiability of the performance measures in numerical computation due to the finite size of integration time step, this paper proposes a regression hybrid method that calculates the shape sensitivity coe?cients of crack speed through polynomial regression analysis based on the sensitivity of atomic responses, which is calculated through analytical shape design sensitivity analysis (DSA). And finally, the proposed method supports for 3D crack propagation problems with periodic boundary condition in one direction. A nano-beam example is used to demonstrate numerically the feasibility, accuracy, and e?ciency of the proposed method.     

两串列扑翼的相位差对平均推力影响机理的实验研究

在一个低雷诺数的循环水洞中,实验研究了前后翅翼之间的相位差对两串列扑翼平均推力的影响.利用一个三分量的Kistler 压力传感器来测量扑翼的瞬时力;利用一个数字粒子测速仪系统(TSI DPIV) 来测量扑翼的前缘涡以及其周围的流场. 当相位差从0° 增加到360°,前翅的平均推力随着相位差正弦变化;前翅平均推力的增加是由于后翅的前缘涡和滞止区域增加了前翅的有效攻角. 后翅平均推力曲线有一个明显的V 字形低谷.低谷处较小的平均推力是由于前翅的脱落涡抑制了后翅前缘涡的形成并且减小了其有效攻角.当间距为0.5倍弦长相位差约为290°时,前后翅翼平均推力系数的合值能达到最大值0.667,明显大于两倍的单翼平均推力系数(2×0.255).      

Unfolding of multiparameter equivariant bifurcation problems with two groups of state variables under left-right equivalent group

Introduction Intheunfoldingtheoryofbifurcationproblems,Refs.[1-6]providedvariousversionsof theversalunfoldingtheorem.Itispointedoutthattheequivalentrelationadoptedintheabove mentionedreferencesiscontactequivalencederivedfromthesingularitytheoryofsmoothmap…     

软弱顺倾岩体爆破层裂的准静态力学模型应用研究

针对顺倾岩质边坡爆破引起软弱夹层冲刷、压密而影响边坡稳定的问题,应用爆轰气体等熵绝热膨胀理论,建立深孔爆破过程中软弱顺倾边坡的准静态力学模型,导出了爆炸作用在软弱夹层内形成爆腔后的准静态压力和软弱层临界层裂长度计算公式。通过分析爆轰气体楔入层面内对边坡岩体产生的抬动作用,推得了边坡潜在滑体的稳定系数与装药参数、岩体力学参数和边坡几何尺寸的定量关系。将提出的准静态力学模型应用于两个典型顺倾岩质边坡的爆破动力稳定分析,得到了与工程实际相符合的计算结果。     

Finite element analysis of edge lamination during hot rolling process of aluminium alloy

Summary The rigid-plastic finite element method is applied to the analysis of the three-dimensional deformation behaviour, in particular the forming of edge lamination during the multi-pass hot roughing process of aluminium. the calculation is carried out for various rolling conditions and reduction schedules, and their influence on the edge lamination is examined. The results suggest that the crop loss due to the edge lamination can be reduced by increasing the roll diameter, the reduction per pass and the initial width of the slab.