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用有限元法计算飞秒激光双光子成型点弹性模量 总被引:1,自引:0,他引:1
采用有限元法对材料为SCR500的飞秒激光双光子成型点力学性能进行建模及仿真计算,得出了不同弹性模量下成型点与探针之间的作用力.进而利用原子力显微镜接触模式,选用无针尖探针,测量了成型点的力学性能,得出了相同位移载荷下成型点与探针之间的作用力.将测量结果和仿真结果进行比较,推算出成型点的弹性模量.分析结果表明。双光子固化成型点的弹性模量大约为宏观材料弹性模量的1/7.这为进一步研究双光子飞秒激光加工微器件的力学性能提供了基础. 相似文献
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C. Bassindale X. Wang W.R. Tyson S. Xu 《Fatigue & Fracture of Engineering Materials & Structures》2018,41(2):494-499
Stress intensity factor solutions for clamped single edge notched tension (SENT) specimens, including a closed‐form function recently proposed by Zhu along with a function by CanmetMATERIALS referenced in the British Standard BS 8571, have been assessed. Solutions for an SENT specimen with a daylight‐to‐width ratio of 10 have been compared with new finite element results generated in this work to assess their accuracies. The results of this study show that the polynomial proposed by Zhu differs by no more than 0.23% compared with the numerical results over the range of 0.2 ≤a/W ≤ 0.7. The CANMET function differs by no more than 0.69% over the same range. 相似文献
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Jeong‐Ho Kim Glaucio H. Paulino 《International journal for numerical methods in engineering》2002,53(8):1903-1935
This paper is directed towards finite element computation of fracture parameters in functionally graded material (FGM) assemblages of arbitrary geometry with stationary cracks. Graded finite elements are developed where the elastic moduli are smooth functions of spatial co‐ordinates which are integrated into the element stiffness matrix. In particular, stress intensity factors for mode I and mixed‐mode two‐dimensional problems are evaluated and compared through three different approaches tailored for FGMs: path‐independent J*k‐integral, modified crack‐closure integral method, and displacement correlation technique. The accuracy of these methods is discussed based on comparison with available theoretical, experimental or numerical solutions. Copyright © 2001 John Wiley & Sons, Ltd. 相似文献
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P. Ma R. K. L. Su W. J. Feng Y. S. Li 《International journal for numerical methods in engineering》2015,103(2):94-113
This paper studies the static fracture problems of an interface crack in linear piezoelectric bimaterial by means of the extended finite element method (X‐FEM) with new crack‐tip enrichment functions. In the X‐FEM, crack modeling is facilitated by adding a discontinuous function and crack‐tip asymptotic functions to the classical finite element approximation within the framework of the partition of unity. In this work, the coupled effects of an elastic field and an electric field in piezoelectricity are considered. Corresponding to the two classes of singularities of the aforementioned interface crack problem, namely, ? class and κ class, two classes of crack‐tip enrichment functions are newly derived, and the former that exhibits oscillating feature at the crack tip is numerically investigated. Computation of the fracture parameter, i.e., the J‐integral, using the domain form of the contour integral, is presented. Excellent accuracy of the proposed formulation is demonstrated on benchmark interface crack problems through comparisons with analytical solutions and numerical results obtained by the classical FEM. Moreover, it is shown that the geometrical enrichment combining the mesh with local refinement is substantially better in terms of accuracy and efficiency. Copyright © 2015 John Wiley & Sons, Ltd. 相似文献
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利用有限元分析软件ANSYS,通过变化栅宽、沟宽及栅极位置等因素,模拟了共面栅探测器在不同的电极设计时的电势分布,并讨论了电极分布不对称时所产生的边缘对感应信号的影响,显示了具有优化设计的共面栅电极,可以进一步提高探测器的能量分辩率。 相似文献
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A. KTARI N. HADDAR A. KOSTER A. MARIE‐LOUISE TOURE 《Fatigue & Fracture of Engineering Materials & Structures》2011,34(7):498-509
Thermal fatigue experiments have been carried out on a single‐edge wedge specimen of the SiMo cast iron to reproduce the conditions experienced by exhaust manifolds during operation. The leading edge temperature was cycled between 20 and 750 °C and the temperature distribution on the specimen surface was measured by thermocouples throughout the thermal cycle. Due to the complexity of the loading and interaction effects between cracks, numerical simulation of crack propagation and shielding effects in multicracked structures appear a useful way to analyze this problem. Therefore, 3D thermo‐mechanical computation was performed with the finite element code ABAQUS of both un‐cracked and multicracked specimen. This computation allowed us to assess the temperature, stresses and strains distribution over a thermal fatigue specimen and the estimation of the crack growth rate using the energy criteria based on the calculation of the J‐integral crack tip. 相似文献
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《Advanced Composite Materials》2012,21(4):343-358
Titanium matrix composites (TMCs) is considered as a candidate material for landing gear structures of the aircraft, which requires the damage tolerant consideration. In order to investigate the damage behavior of SiC-fiber/titanium matrix composites subjected to foreign object impact, low-velocity impact experiments are conducted. Finite element modeling to simulate the damage behavior of TMCs is developed considering the plastic deformation and the damages. Numerical results of mechanical response and damage behavior are compared with experimental results. It is shown that the developed modeling can capture the impact damage of TMCs. In the last part of the present study, a prototype of TMC landing gear structure is fabricated. Impact damage behavior and residual compressive strength are evaluated, and the results are compared with numerical simulation. 相似文献
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Z. He A. Kotousov F. Berto 《Fatigue & Fracture of Engineering Materials & Structures》2015,38(7):860-869
The stress intensity factor (SIF) distribution along the front of a through‐the‐thickness crack is significantly influenced by the presence of the 3D corner (vertex) singularities. All past 3D finite element studies indicated that for mode I, SIF rapidly decreases near the free surface and for mode II, it sharply increases. From the previous numerical simulations, it is unclear what the limiting values of SIF near the surface are and whether these values are infinite or bounded at the vertex point. In this paper, we conduct a careful finite element study and propose a theoretical equation, which describes the SIF behaviour near the vertex. We demonstrate that the asymptotic behaviour of SIF near the surface is governed by the difference in the strength of the corner and edge singularities. Furthermore, we validate our numerical approach and calculations by utilising the invariant properties of J‐integral. 相似文献
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为了进行压电陶瓷材料发电性能测试与研究,研制了一套悬臂梁压电振子发电系统.设计了悬臂梁压电振子,并对压电振子进行了有限元分析和电导测试.在此基础上,设计了能量存储电路,并在低频下对悬臂梁压电振子发电性能进行了实验研究.研究结果表明,当悬臂梁压电振子处于谐振频率状态下振动时,输出电压和功率达到最大.输出电压随着负载的增大而增大,输出功率并不随着负载的增大而增大;压电振子存在-个最佳阻抗,当负载与最佳阻抗匹配时,此时压电振子的能量转化效率最高且输出功率最大.利用本实验系统进行压电发电实验测试,当负载为50 kΩ时,压电振子输出电压为7 V;当负载电阻为15 kΩ时,此时的输出功率最大可达到1.4 mW,产生的功率可以满足无线传感器等低耗能产品的供能需求. 相似文献
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利用超声波断口图技术对不同类型的带单侧贯穿裂纹的PMMA试件进行了测试,得到试件断口上的超声波线。基于ANSYS软件的有限元分析,计算了试件的三维J积分,得到的试件在不同裂纹长度下的三维J积分与它们断口图上的超声波线的形状和凸凹方向相似,将试件扩展裂纹前缘由直线调整为特定曲线后,计算出的三维J积分趋向常量,证实了扩展裂纹前缘的任一点,J积分矢量的幅值都是相同常量的假设。 相似文献
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采用ADAMS分析软件对条烟配送笼车在主副笼叠加运输方式中的载荷进行了分析,得到主笼车在设定条件下的最大载荷值。在此基础上,利用有限元分析软件对主笼车进行应力和形变计算,结果表明,现有的笼车强度和刚度均有较大的设计裕量,可对其进行轻量化设计。按照方管设计的国家标准,通过减薄钢管壁厚进行了减量化设计,并对其进行了应力和形变分析。对比分析结果可知,对笼车开展的轻量化设计,不仅可以满足现有条烟配送运输要求,同时节约了笼车的制造成本,减轻了配送运输过程中的空载质量,有效地提高了运输效能,减小了运输能耗。 相似文献
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A simplified micromechanical model is proposed to estimate the macroscopic mechanical properties of continuous bidirectional-fiber-reinforced composites (CBFRCs) by ignoring Poisson's effect. The model is validated by results from a homogenized finite element approach. Based on the proposed analytical model, the influences of the ratios of fiber/matrix modulus and the fiber volume ratio on the effective modulus and the tensile strength are specifically investigated. The suggested theoretical method provides a convenient tool for estimating the effective mechanical behaviors of CBFRCs, which can be expressed as a function of fiber volume fraction and material parameters. 相似文献
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Y. Huang W. Zhou E. Wang 《Fatigue & Fracture of Engineering Materials & Structures》2014,37(10):1101-1115
Three‐dimensional (3D) finite element analyses are carried out on single‐edge bend [SE(B)] specimens for which the J‐integral resistance curves (J–R curves) have been experimentally determined to develop the constraint‐corrected J–R curves for the X80 grade pipe steel. The constraint parameters considered in this study include QHRR, QSSY, QSSY_m, QLM, QBM1, QBM2, A2, h and Tz. The constraint‐corrected J–R curves were developed on the basis of the constraint parameters obtained from finite element analysis and experimentally determined J–R curves associated with deeply cracked and medium‐cracked SE(B) specimens and validated against shallow‐cracked SE(B) specimens. The analysis results indicate that all the constraint parameters considered in this study except QHRR, QSSY, QSSY_m and QLM lead to reasonably accurate constraint‐corrected J–R curves if the crack extensions are relatively small (≤0.7 mm). For larger crack extensions (≤1.5 mm), the QBM1‐based constraint‐corrected J–R curve leads to the most accurate predictions of J among all the constraint parameters considered. 相似文献
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B. HAKIMELAHI N. SOLTANI 《Fatigue & Fracture of Engineering Materials & Structures》2010,33(10):661-672
In the analysis of fracture mechanics of structures using three‐dimensional (3D) J‐integral, an integral evaluation of line and surface is required. However, because surface integral evaluation requires the calculation of the second derivative of displacement field and commercial finite element codes cannot calculate it, then this portion of the integral is neglected in some research. In this paper, a method for computing 3D J‐integral is presented using finite element analysis. In the analysis, the second derivative evaluation of displacement field is employed. The method is implemented in calculating the J‐integral of some 3D cracks and results are compared to well‐known reference values. The results show that the method is reliable and is suitable for applications in engineering. The portion of 3D J‐integral, namely the surface integral value is investigated and it is shown that neglecting this portion can introduce considerable error in the final results. 相似文献
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L. Saucedo‐Mora C. Zou T. Lowe T. J. Marrow 《Fatigue & Fracture of Engineering Materials & Structures》2017,40(5):683-695
A cohesive element numerical model, which reproduces the three‐dimensional microstructure of a 2.5‐dimensional silicon‐nitrogen‐oxide fibre/fabric‐reinforced boron nitride ceramic matrix composite (SiNO/BN) is applied to simulate the failure of specimens that are observed in situ during diametral compression testing. Measurements of deformation by image correlation of two‐dimensional optical surface observations and three‐dimensional X‐ray computed tomographs are used to fit the simulation's elastic properties for the matrix and fibre tows. The observed patterns of damage nucleation and propagation are correctly simulated using a local tensile strain criterion. 相似文献
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Y. KURONUMA Y. SHINDO T. TAKEDA F. NARITA 《Fatigue & Fracture of Engineering Materials & Structures》2010,33(2):87-93
This paper studies the fracture behaviour of cracked carbon nanotube (CNT)‐based polymer composites by a combined numerical–experimental approach. Tensile tests were conducted on single‐edge cracked plate specimens of CNT/polycarbonate composites at room temperature and liquid nitrogen temperature (77 K), and the critical loads for fracture instabilities were determined. Elastic–plastic finite element simulations of the tests were then performed to evaluate the J‐integrals corresponding to the experimentally determined critical loads. Scanning electron microscopy examinations were also made on the specimen fracture surfaces, and the fracture mechanisms of the CNT‐based composites were discussed. 相似文献