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 The Creep Analysis of Simply Supported Circular Plates 简支圆簿板的蠕变分析 短句来源 On the Static Stability and the Free Vibration of a Simply Supported Cylindrical Shell Patrtially Filled with Liquid under an Axial Static Pressure 部分充液简支圆柱壳体轴向静压下的静力稳定性和自由振动 短句来源 Nonlinear Bending of Simply Supported Rectangular Sandwich Plates 简支夹层矩形板的非线性弯曲 短句来源 Solution of Annular Sector Plate Simply Supported under Concentrated load by Fourier──Bessel Series 受集中荷载作用的简支环扇形板比Fourier──Bessel级数解 短句来源 Green Quasifunction Method for Simply Supported Thin Polygonic Plates 简支多边形薄板问题的准格林函数方法 短句来源 更多
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 ASYMMETRIC BENDING OF CORNER-SUPPORTED RECTANGULAR PLATES 角支矩形板的不对称弯曲 短句来源 NONLINEAR FREE VIBRATION AND POSTBUCKLING OF ORTHOTROPIC SHALLOW CYLINDRICAL SHELLS 四边简支正交各向异性圆柱扁壳的后屈曲和非线性振动 短句来源 NONLINEAR ANALYSIS OF TRAPEZOIDAL SHALLOW SHELLS 对称的简支梯形底扁球壳的非线性分析 短句来源 Solution of the Lateral Bending Problem of Clamped Plate and Its Application 固支边界的矩形板在横向载荷作用下弯曲问题的解及其应用 短句来源 LAME EQUATION SOLUTION TO THICK RECTANGULAR PLATE OF SIMPLE SUPPORT 简支矩形厚板的Lame方程解 短句来源 更多

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 This fact is deduced from results about equivariantD-modules supported on the nilpotent cone of. Given integers n,d,e with $1 \leqslant e >amp;lt; \frac{d}{2},$ let $X \subseteq {\Bbb P}^{\binom{d+n}{d}-1}$ denote the locus of degree d hypersurfaces in ${\Bbb P}^n$ which are supported on two hyperplanes with multiplicities d-e and e. Smoothing Minimally Supported Frequency Wavelets: Part II The main purpose of this paper is to give a procedure to "mollify" the low-pass filters of a large number of Minimally Supported Frequency (MSF) wavelets so that the smoother functions obtained in this way are also low-pass filters for an MRA. Smoothing minimally supported frequency wavelets: Part II 更多
 By direct application of the equation of elastica with reference to a clamped-free buckling rod[1], we are able to obtain the elastica of a clamped-hinged compression rod by treating it in two separate parts. A general formula for buckling rod under five different boundary conditions has been derived. It may be available for use in engineering designs. 本文根据[1]文中一端固定一端自由受纵向荷载的压杆屈曲后的弹性线方程,利用分段法建立固定——铰支端受纵向荷载压杆的弹性曲线方程,从而推导出满足五种边界条件的受纵向荷载压杆的统一公式。可提供工程设计参考。 The theory of fracture mechanics is used to analyse the fracture of journal in the hub-arms of helicopter. The fracture properties of 18CrNiWA steel such as the fracture toughness, crack growth speed, threshold values, FATT values, etc. aremeasured. The KI and dS0/dN expressions for the shaft and the cylinder specimens with surface cracks under bending stress are derived, and the critical crack propagation area and residual life expectancy of the journal are discussed and the overhaul period is also suggested.... The theory of fracture mechanics is used to analyse the fracture of journal in the hub-arms of helicopter. The fracture properties of 18CrNiWA steel such as the fracture toughness, crack growth speed, threshold values, FATT values, etc. aremeasured. The KI and dS0/dN expressions for the shaft and the cylinder specimens with surface cracks under bending stress are derived, and the critical crack propagation area and residual life expectancy of the journal are discussed and the overhaul period is also suggested. Structural fatigue tests on the journal show that the results of analysis carried out by the theory of fracture mechanics are satisfactory; 本文应用断裂力学理论系统地分析了直升机浆毂支臂轴颈的断裂问题;测定了18CrNiWA钢的断裂韧度、裂纹扩展速率、门槛值、断口形貌转变温度等断裂参数;给出了圆轴、圆筒表面裂纹在弯曲条件下的应力强度因子K_1和裂纹面积扩展率的表达式;分析了轴颈的临界裂纹面积与剩余疲劳寿命,确定了检修期;浆毂支臂轴颈疲劳实验表明本文的结论是可信的. In this paper the stresses acting upon the hip bone have been studied by meams of the finite element method during standing on both legs and sitting phases. An isoparametric brick element (8 nodes) is used to represent the cancellous bone and a quadrilateral element is used to model the thin layer of the compact bone. The results indicate that the maximum stress under load 60kg is nearly 297kg/cm2 for sitting phase and 97kg/cm2 for standing on both legs phase. 本文使用有限元方法研究了双足站立时与坐位时作用于髋骨上的应力。松质骨用八节点等参数块单元描述,结果为:60kg荷重,坐位时在坐骨支部位的最大应力约为297kg/cm~2;双足站立时在骶髂关节部位的最大应力约为97kg/cm~2。 << 更多相关文摘
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