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1) multilayer cylinder
层合圆柱体
1.
A theoretical model of 3D transient heat conduction in a multilayer cylinder irradiated by high power laser was developed in which the action of air flow around the exterior surface and the compatibilities of both temperature and heat transfer at the interfaces were taken into consideration.
考虑外表面的气流影响和层间温度与传热的协调关系,建立了激光辐照下,层合圆柱体中的三维瞬态热传导解析模型。
2.
Taking the action of air flow around the exterior surface and the compatibility between temperature and heat transfer at the interfaces into consideration,a 3D theoretical model of transient heat conduction in a multilayer cylinder heated rapidly on the surface is developed.
考虑外表面的气流影响和层间温度与传热的协调关系,建立了表面快速加热下,层合圆柱体中的三维瞬态热传导分析模型。
2) cylindrical laminated shell
圆柱形层合壳体
1.
Energy method is applied to study the buckling problem of near surface triangular, elliptical and lemniscated delamination in a symmetric closed cylindrical laminated shell.
应用能量法研究了对称铺层的闭合圆柱形层合壳体的表层局部分层屈曲问题 ;表层分层形式有三角形、椭圆和双纽线 ;分析了母层壳、子层壳的几何参数、物理参数同分层屈曲临界应变值之间的关系 ;给出了子层分层为椭圆的分层扩展的可能发生方向 。
3) laminated cylindrical shell
层合圆柱壳
1.
The vibrating modal analysis of axisymmetrical laminated cylindrical shells with throughout circumference delamination is investigated.
对具环向贯穿脱层的轴对称层合圆柱壳进行振动模态分析。
2.
Based the nonlinear elastic shell theory, the governing equations of motion for axisymmetrical laminated cylindrical shell with delamination were derived.
基于非线性弹性壳理论,建立了考虑脱层接触效应的具轴对称脱层层合圆柱壳的运动控制方程。
3.
The goveming equations for dynamic response of laminated cylindrical shells with orthotropic layers are derived by use of layerwise shell theory, with quadratic interpolation function adopted in shell thickness direction.
应用分层壳理论并在壳厚方向采用二次插值函数推导出正交层合圆柱壳的动力学方程,并得出了简支层合圆柱壳自由振动方程的解,所给出的振动频率与三维分析的结果吻合良好。
4) laminated circular cylindrical shell
层合圆柱壳
1.
The critical buckling loads of viscoelastic laminated circular cylindrical shells under axial compres- sion are investigated within the theory of classic buckling.
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。
5) sandwich cylindrical cavity
夹层圆柱腔体
1.
With the combination of electrorheological fluid and a sandwich cylindrical cavity, the dynamic and acoustic characteristics, as well as the change of the structural responses, of a sandwich structure while being excited by high frequency noise inside are studied experimentally in this paper.
采用电流变流体(ERF),结合工程实际中常见的隔声腔体结构,通过实验研究了高频声激励作用下含电流变材料夹层圆柱腔体的声振响应特性及其变化。
6) stiffened laminated shells
加筋层合圆柱壳
1.
The dynamics equations of viscoelastic stiffened laminated shells were deduced by means of the mixed layerwise theory and Ressiner′s mixed variational theorem,in which quadratic functions for displacement and three-order or four-order functions for transverse stress in the shell-thickness direction were adopted.
采用混合分层理论和Ressiner混合变分原理,在壳的厚度方向取二次插值函数来描述位移沿厚度方向的变化规律;采用三次和四次插值函数来描述横向应力沿厚度方向的变化,线形处理筋条的变形,推导出粘弹加筋层合圆柱壳的动力学方程和协调方程组,并采用拉普拉斯变换,得出简支粘弹加筋层合圆柱壳稳态振动的响应解。
补充资料:纵向磁场中的单层空心超导圆柱体
纵向磁场中的单层空心超导圆柱体 (singlehollowsuperconductingcylinder(SSC)inalongitudinalmagneticfield)
平行于柱轴(纵向)磁场H0中的单层空心超导长圆柱体(SSC)是复连通超导体。设柱体内外半径分别为r1,r2(r1<r<r2),厚度d=r2-r1,ζ=r/δ,Δ=d/δ,δ=δ0/ψ,δ0,ψ分别为大样品弱场穿透深度和有序参量。由GL理论,徐龙道和Zharkov研究了一系列物性,其中对厚壁样品,磁场难于透入中空部分而只存在原有的量子化冻结磁通。对`\zeta_1\gt\gt1`和$\Delta\lt\lt1$的薄壁样品,腔内磁场H1和样品磁矩M分别为:
$H_1=\frac{H_0 (n\phi_0//\pir_1^2)\zeta_1\Delta//2}{1 (\zeta_1\Delta//2)}$
$M=-\frac{r_2^2\zeta_1\Delta(H_0-n\phi_0//\pir_1^2)}{8[1 (\zeta_1\Delta//2)]}$
这里n为磁通量子数,φ0=h/2e=2.07×10-15Wb。是磁通量子,h和e分别为普朗克常数和电子电荷量。若原先空腔中无冻结磁通(n=0),则腔中磁场是外场H0穿透进入。若$\zeta_1\Delta\lt\lt1$,则H1≈H0,磁场可几乎全穿透到空腔。薄壁不起屏蔽磁场的作用。但若$\zeta_1\Delta\gt\gt1$,则H1≈1,所以虽然$d\lt\lt\delta$,但外场仍难于进入空腔而被壁所屏蔽,称ζ1Δ/2为纵向外场中单层空心长圆柱体的屏蔽因子。对M也可作同样分析。与实心超导小样品类似(见“超导薄膜”),可用与ψ(对坐标的平均),H0,n,温度T和样品尺寸l有关的超导-正常两相吉布斯自由能密度之差$fr{F}(\psi,p)$用GL理论来进行研究分析相变行为及其他一系列物性,如各种临界磁场,临界尺寸等等。这里H0,n,T和l在$fr{F}$宗量中统一记写为p来表示。SSC系统的一、二级相变见图1。随着H0或T的增加,图线由1逐渐上升到4和5。图1(a)的1,2,3三曲线在ψ>0上存在$fr{F}<0$的极小值,超导态是稳态,在3与4曲线之间可有$fr{F}>0$和ψ>0的极小值(图中未画出),则超导态是亚稳的过热(sh)态。曲线4上有$fr{F}>0$,ψ>0的拐点,是超导态的过热边界。稍上,样品即跳跃到ψ=0的正常态或量子跃迁到不同n值的ψ>0的超导态。再往上,如图线5,$fr{F}$的最小值在ψ=0,样品完全处于正常态。相反过程,减小H0或T,图线由5的处于ψ=0的稳定正常态,并维持ψ=0到图线4,在图线3上,极大值在$fr{F}>0$和极小值在$fr{F}<0$与ψ>0处,此时ψ=0的正常态是亚稳的过冷(SC)态。继续减小H0或T,在极大值开始消失只存在极小值时,ψ=0的正常态是过冷边界。再往下,样品处于完全的超导态。由于有过热和过冷滞后现象,相变属一级相变。图1(b)则无滞后现象,相变属二级相变。
Arutunian和Zharkov在此基础上又细致地作了进深的一系列研究,例如所给出的图2(a),这里取T=0K的相干长度ξ0=1×10-7m,GL参量K=0.2,r1=6×10-7m,r2=8×10-7m,图中t=T/Tc,φa1=πr12H0/φ0,φtc表示在图1(a)上拐点所对应的量,用箭头所指表示,实线是过冷边界φsc,虚线是过热边界φsh,平方规律的包络线类同于图2(b)的块样品的热力学临界磁场Hc(T)的相图曲线,但图2(a)体现了外场穿透薄壁而形成磁通量子的跃入空腔的过程和滞后现象。又例如对二级相变的比热随外场和量子数n跃迁振荡情形见图3。图中$bar{c}=\Deltac//c_0$,Δc=cs-cn,c0=μ0Hcn2(0)/Tc,μ0为真空磁导率,Hcn(0)是T=0K时对应于n的热力学临界场,cs和cn分别是超导态和正常态的比热。图3(a)(实线)和(b)(虚线)分别是对应清洁和脏超导体薄壁样品的。在n超导态磁通跃迁进入n±1超导态过程中经历有正常态时,则进入n±1超导态称超导态的重入,或一般地进入正常态后又进入超导态也称超导态的重入。
说明:补充资料仅用于学习参考,请勿用于其它任何用途。
参考词条
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