集中载荷作用下FRP布加固带裂缝木梁的弯曲

将FRP布视为正交各向异性材料,考虑其拉伸与压缩时的双弹性模量性质,给出了四周粘贴FRP布加固带裂缝木梁四点弯曲的边值问题,得到了FRP布加固木梁挠度的解析解,并验证了其有效性和适用性.参数分析表明:相比于侧面粘贴CFRP布,在木梁受拉侧沿轴向粘贴CFRP布的刚度加固效果更加显著;CFRP布加固木梁的挠度随CFRP加固布厚度和弹性模量的增加而减小,但当侧贴CFRP布厚度增加到某一值时,继续增加厚度对木梁挠度的减少效果已不明显;当受拉侧CFRP布厚度较小时,木梁挠度随CFRP布厚度的增加非线性减小,而当受拉侧CFRP布厚度较大时,木梁挠度随CFRP布厚度几乎呈线性减小.同时,当侧贴CFRP布的剪切模量很大时,此时,CFRP布加固带裂缝木梁的挠度趋于CFRP布加固完整无裂缝木梁的挠度,此时,CFRP加固完全消除了裂缝因素.     

Nonlinear aeroelastic stability analysis of wind turbine blade with bending–bending–twist coupling

In this study, the nonlinear aeroelastic stability of wind turbine blade with bending–bending–twist coupling has been investigated for composite thin-walled structure with pretwist angle. The aerodynamic model used here is the differential dynamic stall nonlinear ONERA model. The nonlinear aeroelastic equations are reduced to ordinary equations by Galerkin method, with the aerodynamic force decomposition by strip theory. The nonlinear resulting equations are solved by a time-marching approach, and are linearized by small perturbation about the equilibrium point. The nonlinear aeroelastic stability characteristics are investigated through eigenvalue analysis, nonlinear time domain response, and linearized time domain response.     

三点起爆形成尾翼EFP的数值模拟和实验研究

利用LS-DYNA软件对三点起爆形成尾翼EFP的过程进行了数值模拟,深入研究了爆轰波传播过程中的波形结构和强度的变化规律以及药型罩材料在复合爆轰波作用下驱动变形的特性和规律,加深了对三点起爆条件下药型罩形成带尾翼EFP机理的认识。在此基础上,设计了三点同步起爆装置和EFP装药进行实验。研究结果表明:设计的三点起爆装置作用可靠,满足三点起爆EFP装药的设计要求;形成的EFP弹形稳定,与计算结果吻合较好;尾翼EFP飞行过程中的速度降减小,稳定性提高。     

弹性半空间地基上圆形基础板的位移场和应力场

针对弹性半空间地基上圆形基础底板的弯曲问题,根据地基土壤的受力特性和已有实验研究成果,假设圆形基础底板底部与地基土壤之间是由竖向集中荷载引起的接触应力分布形式,采用板的弯曲理论和通过数值积分及最小二乘法拟合的方法,推导出完全满足边界条件的弹性半空间地基上圆形基础底板上部受集中力作用、下部受幂函数形式连续分布荷载作用时的位移场、径向和环向应力场的表达式。尽管圆形基础板属于中厚度板,但是该表达式的计算精度和可靠性得到了有限元分析软件ANSYS验证。     

低速冲击下泡沫金属填充薄壁圆管的弯曲行为

采用实验方法研究了低速冲击下泡沫金属填充薄壁圆管的弯曲行为,详细说明了实验方法和原 理。通过与准静态实验结果的比较发现,冲击加载使泡沫金属填充圆管跨中截面的局部压入变形增大,跨中 截面高度变小,结构下缘拉裂破坏延迟。由于结构的惯性效应,锤头总冲击力高于准静态加载时的对应值。     

基于平板振动精确化方程求解动应力集中问题

基于文献[8]给出的平板弯曲振动精确化方程,对含圆孔平板中弹性波散射与动应力集中问题进行了研究.文中给出了分别基于Mindlin板与精确化板方程在不同参数下圆孔动弯矩集中系数的数值结果,并对结果进行了对比分析和讨论.结果表明:在较低频率和薄板情况下,基于文献[8]的方程与基于Mindlin板理论得到的动弯矩结果是基本一致的;在较高频率和厚板情况下,基于文献[8]的方程与基于Mindlin板理论的动弯矩结果相差较大,最大值超出可达16%.由于文献[8]给出的平板振动精确化方程是在没有任何工程假设条件下得到的,因此其分析计算结果更精确一些.      

考虑中性层位置变化的微悬臂梁气体传感器静态模型的分析

微悬臂梁是一种高灵敏度的生化传感器。本文考虑吸附表面应力引起的中性层位置的变化,采用能量法建立了微悬臂梁在单层分子吸附稳定后的静态弯曲模型,并以表面吸附有水蒸汽分子的微悬臂梁为例,研究了微悬臂梁曲率半径随其厚度、杨氏模量及吸附分子间距的变化规律以及中性层位置变化对微悬臂梁传感器性能预测的影响,结果发现：1)微悬臂梁的曲率半径与其杨氏模量、厚度及吸附分子间距之间可以近似用一次、二次和八次函数关系表示;2）中性层变化导致的曲率半径计算误差,随着微悬臂梁厚度、杨氏模量的增加而减小,但影响较小,而吸附分子间距会对该相对误差产生明显影响;3）中性层位置变化会对微悬臂梁传感器灵敏度和表面应变预测产生明显的影响。     

Concentration‐dependent Raman study of noncoincidence effect in the NH2 bending and CO stretching modes of HCONH2 in the binary mixture (HCONH2 + CH3OH)

The isotropic and anisotropic parts of the Raman spectra of NH₂ bending and ν(CO) stretching modes of HCONH₂ in a hydrogen‐bonding solvent, methanol, at different concentrations have been analyzed carefully in order to study the noncoincidence effect (NCE). In neat HCONH₂, the experimentally measured values of noncoincidence Δν_nc are ∼11 and ∼18 cm⁻¹ for the NH₂ bending and ν(CO) stretching modes, which reduce to 0.45 and 1.14 cm⁻¹, respectively at the concentration of HCONH₂ in mole fraction, χ_m = 0.1. The experimental results have been explained on the basis of two models, namely, the microscopic prediction of Logan and the macroscopic model of Mirone and Fini. The relative success of the two models in explaining the experimental data for both the modes have been discussed. It has been observed that in case of the ν(CO) stretching vibrational mode the Logan model can reproduce the experimental data rather precisely, whereas in the case of the NH₂ bending mode, Mirone and Fini model yields more accurate results. Copyright © 2006 John Wiley & Sons, Ltd.     

Large bending behavior of creased paperboard. II. Structural analysis

The mechanics of a paradigmatic typical carton corner with five creases is analyzed theoretically, in closed form. A general kinematical analysis of the mechanism (in finite rotation) is presented, assuming the versor of the intermediate crease, s, as a 2-degree-of-freedom Lagrangian parameter. The rotation θ_c of the cth crease is derived, together with the existence domain and a discussion of the singular configurations.The actions, driving the carton during a prescribed quasi-static erection program, are derived in a very efficient manner using the Virtual Works Equation, taking into account a non-linear anholonomic bending constitutive law of the creased paperboard. In particular, the active and reactive components of the moment ?, driving s along its path, are identified. No resort to the tangent stiffness computation is required. Some numerical examples illustrate the rotation and the driving forces obtained for both monotone-loading and complex loading–unloading erection paths.The presented results, “exact” within the scope of the restrictive hypotheses assumed, may be used in a preliminary design approach as well as a benchmark for more realistic FEM or CAE simulators.     

变厚度正交各向异性矩形板非线性非对称弯曲问题的基本方程

在不计体力,考虑了薄膜力引起在z方向的分力,导出了厚度线性变化的正交各向异性矩形板非线性非对称弯曲问题的本构方程;在引进无量纲变量和引入三个小参数的条件下,给出了挠度函数W(x,y)和应力函数Φ(x,y)的无量纲化的支配方程形式．