热效应对静不定梁热弯曲的影响

建立了静不定梁在温度场中热弯曲的微分方程,推导出了在小挠度变形条件下静不定梁热弯曲的挠曲线表达式.研究结果表明:当温度沿梁高呈线性分布时,梁的温度使静不定梁受到轴向热力作用,梁底与梁顶的温度差使静不定梁发生热弯曲.在小挠度变形条件下:考虑轴向热力的作用时,静不定梁的热弯曲是非线性问题;忽略轴向热力的作用时,静不定梁的热弯曲是线性问题.Timoshenko的名著《材料力学》,在研究两端固支梁热弯曲问题时,得到了"两端固支梁热弯曲挠曲线表达式有时是意想不到的"结论,即两端固支梁热弯曲挠曲线表达式为零的结论.因此在考虑轴向热力对静不定梁热弯曲影响的基础上,研究了静不定梁热弯曲问题,把两端固支梁热弯曲问题与其他静不定梁热弯曲问题进行对比,对两端固支梁热弯曲挠曲线表达式为零的结论进行了理论解释,可知两端固支梁在热状态下的变形是一个弹性稳定问题.     

用切比雪夫多项式研究短梁的弯曲计算

考虑剪切效应,利用切比雪夫多项式构造严格满足表面切应力边界条件的轴向位移表达式,建立了短梁弯曲问题的新理论．利用奇异函数把作用在短梁上的复杂外载荷表示为分布载荷,推导出了短梁弯曲时的截面正应力公式及挠曲线表达式．把采用切比雪夫多项式推导出短梁的弯曲计算公式计算结果与弹性理论计算结果进行比较,可知该方法的计算精度较高．研究结果表明：在复杂外载荷作用下,当长高比小于等于6时,剪切变形对梁的弯曲挠度影响较大,而当长高比小于3时,剪切变形对梁的弯曲应力影响较大;因此建议采用切比雪夫多项式方法给出的挠度表达式、弯曲应力进行计算,因为切比雪夫多项式方法不但给出了复杂外载荷作用下梁截面挠度、弯曲应力的计算通式,而且该方法具有计算过程简便、精度高的优点．     

热荷载作用下Timoshenko功能梯度夹层梁的静态响应

在精确考虑轴线伸长和一阶横向剪切变形的基础上建立了Timoshenko功能梯度夹层梁在热载荷作用下的几何非线性控制方程.采用打靶法数值求解所得强非线性边值问题,获得了两端固支功能梯度夹层梁在横向非均匀升温作用下的静态热过屈曲和热弯曲变形数值解.分析了功能梯度材料参数变化、不同表层厚度和升温参数对夹层梁弯曲变形、拉-弯耦...     

轴向扩散下简支饱和多孔弹性梁的大挠度分析

基于多孔介质理论和弹性梁的大挠度理论,并考虑轴向变形,在孔隙流体仅沿轴向扩散的假设下,建立了微观不可压饱和多孔弹性梁大挠度弯曲变形的一维非线性数学模型.在此基础上,忽略饱和多孔弹性梁的轴向应变,并利用Galerkin截断法,研究了两端可渗透的简支饱和多孔弹性梁在突加横向均布载荷作用下的拟静态弯曲,给出了饱和多孔梁弯曲时挠度、弯矩和轴力以及孔隙流体压力等效力偶等沿轴线的分布曲线.揭示了大挠度非线性和小挠度线性模型的结果差异,指出大挠度非线性模型的结果小于相应小挠度线性模型的结果,并且这种差异随着载荷的增大而增大.计算表明:当无量纲载荷参数q>5时,应该采用大挠度非线性数学模型进行研究.     

简支饱和多孔弹性梁的非线性弯曲

基于饱和多孔介质理论和弹性梁的大挠度弯曲假设,在多孔弹性梁轴线不可伸长,孔隙流体仅沿轴向方向扩散的限制下,建立了微观不可压饱和多孔弹性梁大挠度拟静态响应的一维非线性数学模型.在此基础上,利用Galerkin截断法,分析了两端可渗透的简支多孔弹性梁在突加横向均布载荷作用下的非线性弯曲,给出了梁弯曲时挠度、弯矩以及孔隙流体压力等效力偶随时间的响应曲线.数值结果表明:当载荷较小时,大挠度非线性与小挠度线性理论的结果相差很小,而当载荷较大时,非线性大挠度理论的结果小于相应线性小挠度理论的结果,并且这种差异随着载荷的增大而增大.同时,在载荷突加于梁上时,多孔弹性梁骨架起初不变形,孔隙流体压力等效力偶由零突增为非零,其值与外载荷保持平衡.随着时间的增加,梁的挠度增加,等效力偶逐渐减小为零,最终多孔梁骨架承担全部的外载荷.     

不可压饱和多孔弹性简支梁的动力响应

在杆件弯曲小变形的假定下,考虑杆件的侧向变形因素,根据多孔介质理论,本文首先建立了不可压饱和多孔弹性梁弯曲变形时动力响应的控制方程。其次,基于所建立的控制微分方程,利用变量分离法,研究了两端可渗透的饱和多孔弹性简支梁在梁中间集中载荷作用下的动力响应,得到了不同物性参数下简支梁动态弯曲时挠度和孔隙流体压力等效力偶等随时间的响应曲线。研究发现由于孔隙流体和固相骨架的相互作用,不可压饱和多孔弹性梁挠度的动力响应具有粘性特征,同时,随着时间的增加,饱和多孔弹性梁的挠度、弯矩等最终趋于经典弹性梁的静挠度、弯矩,此时,孔隙流体压力为零,梁的固相骨架承担所有的外载荷。     

铝面板PMI泡沫芯夹层梁弹性弯曲的二维模型

将面板PMI泡沫芯夹层梁的弯曲问题按平面应力问题研究,采用弹性理论建立了铝面板PMI泡沫芯夹层梁弯曲变形的微分方程,利用奇异函数把作用在梁上的外载荷表示为分布载荷,推导出了铝面板PMI泡沫芯夹层梁弯曲变形时的挠曲线表达式．采用该方法对面板PMI泡沫芯夹层梁弯曲挠度进行计算,将求得的计算结果与有限元法结果及实验数据进行对比,发现该方法求得的梁中点挠度更接近实验值,这说明该方法可靠的．该方法给出了铝面板PMI泡沫芯夹层梁弯曲时的挠度计算通式,而且梁中点挠度计算公式的表达形式也较为简便,可方便工程设计人员在工程实际中推广应用．     

热载荷作用下梯度多孔材料梁弯曲及过屈曲力学行为的研究

基于Bernoulli-Euler梁理论,引入物理中面解耦了复合材料结构的面内变形与横向弯曲特性,研究了梯度多孔材料矩形截面梁在热载荷作用下的弯曲及过屈曲力学行为．假设沿梁厚度方向材料的性质是连续变化的,利用能量法推导了矩形截面梁的控制微分方程和边界条件,并用打靶法对无量纲化的控制方程进行数值求解．利用计算得到的结果分析了材料的性质、热载荷、边界条件对矩形截面梁非线性力学行为的影响．结果表明,对称材料模型下,固支梁与简支梁均显示出了典型的分支屈曲行为特征,而其临界屈曲热载荷值均会随着孔隙率系数的增加而单调增加．非对称材料模型下,固支梁仍显示出分支屈曲行为特征,但其临界屈曲热载荷不再随着孔隙率系数的变化而单调变化;而对于两端简支梁,发生了弯曲变形,弯曲挠度随载荷的增大而增大．     

饱和多孔弹性Timoshenko梁的大挠度分析

基于微观不可压饱和多孔介质理论和弹性梁的大挠度变形假设,考虑梁剪切变形效应,在梁轴线不可伸长和孔隙流体仅沿轴向扩散的限定下,建立了饱和多孔弹性Timoshenko梁大挠度弯曲变形的非线性数学模型.在此基础上,利用Galerkin截断法,研究了两端可渗透简支饱和多孔Timoshenko梁在突加均布横向载荷作用下的拟静态弯曲,给出了饱和多孔 Timoshenko梁弯曲变形时固相挠度、弯矩和孔隙流体压力等效力偶等随时间的响应.比较了饱和多孔Timoshenko梁非线性大挠度和线性小挠度理论以及饱和多孔 Euler-Bernoulli梁非线性大挠度理论的结果,揭示了他们间的差异,指出当无量纲载荷参数q＞l0时,应采用饱和多孔Timoshenko梁或Euler-Bernoulli梁的大挠度数学模型进行分析,特别的,当梁长细比λ＜30时,应采用饱和多孔Timoshenko梁大挠度数学模型进行分析.     

地基梁动-静态响应的比较分析

采用分离变量法求得了冲击荷载作用下的开尔文地基上两端自由有限长梁动态挠曲线方程的级数解;分析了地基梁结构参数和冲击荷载作用时间对梁挠曲线特征值（最大挠度和挠曲线面积）的影响规律;比较地基梁动态挠曲线与静荷载引起的地基梁静态挠曲线之间差异,发现：(1)等效地基梁动态最大挠度或挠曲线面积的当量静荷载值与冲量之间不存在良好对应关系;(2)依据地基梁动态挠曲线用静态方法反演得到的地基梁结构参数有可能含有较大的偏差．     

湿式发射对同心筒瞬态热冲击的影响机理

针对路基同心筒自力发射整体热环境恶劣的问题,依托弹性变形和域动分层相结合的动网格技术,基于均质多相流理论并耦合液态水专用汽化求解程序,建立在发射筒底部注水的三维气液两相流体动力学模型;以火箭发动机自由射流注水实验为基础,验证汽化程序三维计算的可靠性与有效性;通过瞬态数值计算,讨论筒底注水角度对导弹、内外筒热环境和导弹载荷特性的影响规律。分析表明:发射筒内发生了显著的汽化反应;导弹及发射系统总体热环境得到了显著改善,实现了发射系统持续降温的目的;在筒底注水后,弹底的附加推力及火箭发动机的推力有一定增加,随着注水量的减少,注水对导弹载荷的影响越来越弱。     

Residual stress evolution regularity in thermal barrier coatings under thermal shock loading

Residual stress evolution regularity in thermal barrier ceramic coatings (TBCs) under different cycles of thermal shock loading of 1100°C was investigated by the microscopic digital image correlation (DIC) and micro-Raman spectroscopy, respectively. The obtained results showed that, as the cycle number of the thermal shock loading increases, the evolution of the residual stress undergoes three distinct stages: a sharp increase, a gradual change, and a reduction. The extension stress near the TBC surface is fast transformed to compressive one through just one thermal cycle. After different thermal shock cycles with peak temperature of 1100°C, phase transformation in TBC does not happen, whereas the generation, development, evolution of the thermally grown oxide (TGO) layer and micro-cracks are the main reasons causing the evolution regularity of the residual stress.     

线圈隔热层对光纤陀螺温度误差的影响分析

针对温度变化所引起的光纤陀螺非互易相移误差,详细研究了隔热材料对减小热漂移误差的作用,并详细比较了使用不同厚度隔热层的光纤陀螺在相同变温历程下的热漂移误差大小以及达到热平衡状态所需的时间。仿真结果表明,当隔热层的厚度由0mm变化到4mm的过程中,热漂移误差的峰值由0.12(°)/h降低到了0.08(°)/h,同时达到热平衡的时间从2 520 s增加到了3 600 s。利用该仿真结果,可以在保证热启动时间满足条件的前提下找到一个最优的隔热层厚度,从而使热漂移误差的峰值最小。     

Determining thermal properties of thin coatings using the “thermal mirror” method

We suggest a photothermal method for measuring thermal properties of opaque coatings. The coating–substrate assembly is irradiated by the repetitive pulse power laser which causes a nonstationary buckling of the coating. Thermal properties of the coating are determined by comparing the measured phase shift in the wave component of the temporal dependence of beam deflection angle of the low power laser with theoretical predictions obtained by solving equations of thermal elasticity.     

Axially symmetric thermal stress of an external circular crack under general thermal conditions

Summary The paper presents a solution for the linear thermoelastic problem of determining axisymmetric stress and displacement fields in an isotropic elastic solid of infinite extent weakened by an external circular crack under general mechanical loadings and general thermal conditions. The mechanical loadings and thermal conditions applied on the crack faces are axisymmetric, being non-symmetric about the crack plane. In similar lines of [7], equations of equilibrium of an elastic solid conducting heat have been solved using Hankel transforms and Abel operators of the first kind. Expressions for stress, displacement, temperature and heat flux functions are obtained in terms of Abel transforms of the first kind of the jumps of stress, displacement, temperature and heat flux at the crack plane. Two types of thermal conditions, that is, general surface temperatures and general heat flux on faces of the crack are considered. In both the cases, closed form solutions have been obtained for the unknown functions solving Abel type of integral equations. Explicit expressions for stresses, displacements, temperature fields, stress intensity factors have been obtained. Two special cases of thermal conditions in which: (i) crack faces are subjected to constant non-symmetric temperatures over a circular ring area, (ii) crack faces are subjected to constant non-symmetric heat flux over a circular ring area, have been considered. In some special cases, results have been compared with those from the literature.     

Three-dimensional stretched flow of Jeffrey fluid with variable thermal conductivity and thermal radiation

This article addresses the three-dimensional stretched flow of the Jeffrey fluid with thermal radiation. The thermal conductivity of the fluid varies linearly with respect to temperature. Computations are performed for the velocity and temperature fields. Graphs for the velocity and temperature are plotted to examine the behaviors with different parameters. Numerical values of the local Nusselt number are presented and discussed. The present results are compared with the existing limiting solutions, showing good agreement with each other.     

Study of skin model and geometry effects on thermal performance of thermal protective fabrics

Thermal protective clothing has steadily improved over the years as new materials and improved designs have reached the market. A significant method that has brought these improvements to the fire service is the NFPA 1971 standard on structural fire fighters’ protective clothing. However, this testing often neglects the effects of cylindrical geometry on heat transmission in flame resistant fabrics. This paper deals with methods to develop cylindrical geometry testing apparatus incorporating novel skin bioheat transfer model to test flame resistant fabrics used in firefighting. Results show that fabrics which shrink during the test can have reduced thermal protective performance compared with the qualities measured with a planar geometry tester. Results of temperature differences between skin simulant sensors of planar and cylindrical tester are also compared. This test method provides a new technique to accurately and precisely characterize the thermal performance of thermal protective fabrics.     

Coherent gradient sensing method for measuring thermal stress field of thermal barrier coating structures

Coherent gradient sensing(CGS)method can be used to measure the slope of a reflective surface,and has the merits of full-field,non-contact,and real-time measurement.In this study,the thermal stress field of thermal barrier coating(TBC)structures is measured by CGS method.Two kinds of powders were sprayed onto Ni-based alloy using a plasma spraying method to obtain two groups of film–substrate specimens.The specimens were then heated with an oxy-acetylene flame.The resulting thermal mismatch between the film and substrate led to out-of-plane deformation of the specimen.The deformation was measured by the reflective CGS method and the thermal stress field of the structure was obtained through calibration with the help of finite element analysis.Both the experiment and numerical results showed that the thermal stress field of TBC structures can be successfully measured by CGS method.