共查询到19条相似文献,搜索用时 453 毫秒
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本文研究了复合材料直线型正交各向异性圆板的大挠度弯曲问题。首先通过周向刚度分析建立了非轴对称挠曲函数的形式:然后采用伽辽金法求解卡门方程, 其中应力函数是通过求解其非线性协调方程而精确得到的。由此,对周边固支而径向位移约束和自由两种边界条件求解了几种各向异性性质的复合材料园板;并讨论了非轴对称位移项引起的影响。计算结果表明, 非轴对称位移项的影响随着材料正交各向异性强度的增大而更加显著。当材料刚度系数比E1/E2=40时, 其对挠度的影响可达17%。 相似文献
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超声Lamb波法是检测板状结构损伤的常用方法,然而纤维增强聚合物基复合材料(Fiber reinforced plastics,FRP)本身的各向异性会对Lamb波损伤定位的精度造成较大的影响。为了解决此问题,在传统椭圆法的基础上,提出了考虑材料各向异性的时间概率密度法的损伤定位方法。该方法通过考虑不同传播方向的A0模态波的群速度变化,计算FRP板上任意一点存在损伤的反射波的走时,得到声波传播时间图。创建声波传播时间与实际损伤反射波走时的映射关系,可得到能表征损伤存在概率的时间概率密度图,通过相应的数值分析和实验研究,发现本方法误差比传统椭圆法误差的减小率可达到70%以上,论证本方法对各向异性FRP板损伤定位的可行性和准确性。 相似文献
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对Fe74.1Cu1Nb3Si15B6.9(%,原子分数)纳米晶合金进行连续张力退火,研究了张力退火感生各向异性对纳米晶合金磁性能的影响。结果表明,张力退火产生的感生各向异性常数(Ku)与退火张力(σ)满足线性关系。随着退火张力的增大合金在f =5 kHz和H=3 A/m测试点的有效磁导率(μe)先增大后减小,且随着磁场和频率的提高有效磁导率(μe)的衰减减小。退火张力为67 MPa时有效磁导率(μe)在磁场强度H为0~800 A/m和频率f为1 k~3 MHz范围内保持约800,表现出恒导磁特性。同时,合金的单位质量损耗(Pm)随着退火张力的增大而减小,当退火张力为67 MPa时损耗为68 W/kg (测试条件:Bm=300 mT,f =100 kHz),与无张力退火相比下降约67%。同时,通过磁光克尔效应观察到张力退火后合金内部形成垂直于张力方向的180°片形畴,随着退火张力的增大磁畴宽度减小且趋于一致,退火张力为67 MPa时片形畴的宽度约为85 μm。 相似文献
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装配式H型钢腹板开孔耗能支撑是由腹板开孔H型钢和传力槽钢通过螺栓连接组成的新型耗能支撑,可有效避免支撑构件失稳。为了研究腹板开孔形状对这种支撑的耗能性能的影响,进行了装配式耗能支撑试件低周往复加载试验,并采用有限元软件进行了模拟计算。试验结果表明:装配式H型钢腹板开孔耗能支撑滞回曲线饱满,耗能能力强,变形能力好。在轴向荷载作用下,试件主要依靠开孔腹板孔间板件进入塑性变形耗能阶段,腹板开长圆孔的试件与腹板开椭圆孔的试件孔间板件端部为薄弱部位,腹板开菱形孔的试件孔间板件中间部位为薄弱部位,加载过程中这些部位首先进入塑性变形阶段并最先发生断裂。加载过程中螺栓与槽钢始终处于弹性变形状态。有限元分析表明:改变腹板宽度对于腹板开长圆孔的耗能支撑的承载能力与初始刚度影响最大,对于腹板开椭圆孔的耗能支撑影响最小;改变孔间板件宽度对于腹板开菱形孔的耗能支撑影响较小。改变腹板厚度对于三种腹板开孔形式耗能支撑的承载力与初始刚度影响相近。当试件主体过早失稳,可通过增大高宽比、减小腹板厚度或选用翼缘更大的槽钢来避免。耗能板件螺栓连接部位安全可靠,未见变形或破坏,布置螺栓时孔距不应超过4.5d0。 相似文献
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本文研究了纤维体积含量(Vf)与碳纤维/7740玻璃的相对密度(Ds)抗弯强度(σb)和冲击韧性(ak)之间的关系。用泥浆浸渗法制带及热压成形技术制备试样。实验结果表明:材料的Ds随Vf的增加而降低;σb和ak值开始随Vf的增加而增大,在Vf为40%左右时出现极大值,之后随Vf增加而降低。对Vf为4096样品的σb分布规律进行了分析,表明:其σb服从韦布尔分布。所获材料的最高σb为370Mpa,ak值为31KJm-2。 相似文献
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含缺口受拉平板塑性应力场的有限元分析 总被引:2,自引:0,他引:2
含尖缺口受拉平板三维应力场是断裂分析研究中常遇到的问题,进入塑性状态以后,缺口尖端的应力状态和分布与弹性条件下有很大的不同。通过有限元的方法对含缺口受拉平板的塑性应力场进行了分析,并进一步研究了厚度和缺口半径因素对缺口尖端应力场的影响。分析结果表明,缺口半径减小提高了平面内应力σx和σy,也提高厚度方向应力σz和平面应变系数,平面应变系数在塑性条件下趋于0.5;厚度对平面内应力σx和σy影响很小,但提高厚度方向应力σz和平面应变系数,平面应变系数在载荷较小时趋于材料泊松比μ,在载荷较大时趋于0.5。 相似文献
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An engineering formula for the theoretical stress concentration factor of orthotropic notched plates under tension is provided, as a function of the material elastic constants and the Kt of the corresponding isotropic case. The accuracy and limits of applicability of the new solution are discussed by comparison to data from the literature and results from FE analyses on notched geometries of practical interests. The proposed solution represents a very useful tool to estimate the stress concentration factor of notched orthotropic plates, composite orthotropic laminae, orthotropic unidirectional laminates and homogenised orthotropic composite laminates. 相似文献
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本文建立了一种杂交有限条法,并应用于各向同性板和各向异性板。这工作是基于修正余能原理进行的。在有限条列式的过程中,在条中假设应力场而在条的边界上假设位移场。数值计算表明,过种方法是合理的,能较快地逼近准确解。 相似文献
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对两种材料体系和铺层的复合材料层合板进行低速冲击后压缩强度试验 , 以研究低速冲击后层合板的压缩破坏机理。讨论了表面凹坑深度、 背面基体裂纹长度、 损伤面积以及剩余压缩强度与冲击能量的关系。在试验研究的基础上 , 建立了复合材料低速冲击后剩余强度估算的一种椭圆形弹性核模型。该模型将冲击损伤等效为一刚度折减的椭圆形弹性核 , 采用含任意椭圆核各向异性板杂交应力有限元分析含损伤层合板的应力应变状态 ,并应用点应力判据预测层板的压缩(或压、 剪)剩余强度。理论分析与试验结果对比表明 , 该模型简单有效。 相似文献
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Muhammad Treifi S. Olutunde Oyadiji Derek K. L. Tsang 《International journal for numerical methods in engineering》2009,77(4):558-580
The fractal‐like finite element method (FFEM) is an accurate and efficient method to compute the stress intensity factors (SIFs) of different crack configurations. In the FFEM, the cracked/notched body is divided into singular and regular regions; both regions are modelled using conventional finite elements. A self‐similar fractal mesh of an ‘infinite’ number of conventional finite elements is used to model the singular region. The corresponding large number of local variables in the singular region around the crack tip is transformed to a small set of global co‐ordinates after performing a global transformation by using global interpolation functions. In this paper, we extend this method to analyse the singularity problems of sharp notched plates. The exact stress and displacement fields of a plate with a notch of general angle are derived for plane‐stress/strain conditions. These exact analytical solutions which are eigenfunction expansion series are used to perform the global transformation and to determine the SIFs. The use of the global interpolation functions reduces the computational cost significantly and neither post‐processing technique to extract SIFs nor special singular elements to model the singular region are needed. The numerical examples demonstrate the accuracy and efficiency of the FFEM for sharp notched problems. Copyright © 2008 John Wiley & Sons, Ltd. 相似文献
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The classical assumptions of standard beam theory include that of uniaxial stress for isotropic beams, or vanishing transverse moment for beams of layered orthotropic materials. Wide beams, on the other hand, display the familiar effect in which the transverse “anticlastic” curvature is assumed to vanish. The transition between these behaviors is not well characterized, and is addressed in the present work by means of a solution for orthotropic plates with two free lateral edges, so as to represent a beam of any aspect ratio. It is found that the transition is independent of the thickness, but depends on the length/width aspect ratio and the material properties. The calculations show that the deviation from narrow beam behavior occurs at a length/width aspect ratio of about 10 for isotropic and many orthotropic materials, and depends on the orthotropic material properties. Comparisons with experimental data in the literature support these conclusions. 相似文献
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为了研究叶片表面完整性对其振动疲劳性能的影响,本文模拟分析了某型高温合金叶片在振动疲劳实验过程中的动力学应力响应,获得叶片共振时应力幅值随时间的变化规律,分析了残余应力和粗糙度对叶片振动疲劳寿命和疲劳极限的影响规律.结果表明:叶片共振过程中的应力响应幅值先增大后减小呈周期性变化,属于"拍"现象,满足关系σ=1 046sin(242.83t)sin(5 828t);叶片的振动疲劳极限和疲劳寿命均随残余应力和粗糙度的增大而减小,振动疲劳极限和残余应力之间的关系满足σfat=510.9-0.31-70.93σrest;而疲劳极限和粗糙度之间的关系则满足σfat=9.67R2roughness-70.93Rroughness+713.23. 相似文献
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The stress state in plates with circular holes made of orthotropic homogeneous material has no singularities and it can be
exactly determined. The numerical stress distribution calculation by the finite element method will be compared with those
obtained by the analytical equations developed by several authors. The goal of this work is to validate the finite element
method, in conjunction with in-plane and out of plane failure criteria, in order to calculate not only the stress distribution
for orthotropic plates with circular holes but also to determine their ultimate strength.The tool used has been a user subroutine
(UMAT) specially developed for this work that implements the features of the commercial FE program (ABAQUS). The code performs
an implicit analysis of the stress-state with progressive damage modelling.Finally, both of them, numerical and analytical
method, will be checked with experimental tests by means of strain gauges. 相似文献