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51.
为了进一步研究疲劳裂纹在萌生阶段的特点,本文结合数字图像相关方法 (Digital Image Correlation Method,DIC)设计并组建了配合液压疲劳试验机加载的原位观测系统。同时针对DIC测量方法中的关键技术进行研究,分别提出了一种可应用于视场宽度2mm下DIC计算的微小散斑制备方法,以及空间调节方法以提高试验可靠性。最后应用该系统开展针对航空发动机火焰筒材料GH536的微裂纹自然萌生试验。通过采取两种不同的DIC分析策略,分别获得疲劳过程中的总应变幅以及最大累积塑性应变的演化规律。结果表明总应变幅演化可确定自然萌生裂纹位置,最小可识别50μm裂纹;最大累积塑性应变分析可得萌生寿命占比约85%,并在裂纹出现后塑性应变急剧增加。 相似文献
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用CT图像分析C/C复合材料的内部缺陷 总被引:4,自引:5,他引:4
总结了不同类型三向增强C/C复合材料CT检测图像及其对应的内部缺陷,结果表明:CT技术主要缺陷区与正常区存在的密度差异,对C/C复合材料内部进行质量检测,但在某些特定条件下,相同种类的缺陷可能表现出不同的CT图像,不同种类缺陷可能产生类似的CT图像,缺陷类型的判定必须与其它检测手段相结合才可确定,CT检测也有可能漏检部分缺陷。 相似文献
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This investigation studies the effect of trailing-edge scalloping on the lift and drag force coefficients of flat, membrane wings that vibrate at low Reynolds numbers (<61,000). A series of rigid, flat plate frames with moderate aspect ratio and repeating membrane cell structure were studied and compared to a rigid plate and a rigid scalloped plate. Lift and drag measurements were acquired using an external force-balance; flow fluctuation measurements were captured with a hot-wire. Results showed that the size and aspect ratio of the latex cell had a greater impact on lift than scalloping and that scalloping had a greater effect on drag than the cell aspect ratio. Compared to the solid wings, the membrane wings exhibited higher lift and drag coefficients, likely due to both effective cambering and dynamic interaction with the free shear layer. While trailing-edge scalloping decreased both the lift and drag coefficients relative to no scalloping, the greater effect was on drag, thus, increasing aerodynamic efficiency. The maximum lift-to-drag ratio was attained for a 25% scallop with a repeating cell aspect ratio of one. A unique nondimensional scaling of the membrane vibration peak frequency is also presented. 相似文献
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为了提升不完全角度计算机断层成像(CT)图像的重建精度和重建效率,研究了有限角度和稀疏角度下的CT图像重建问题,提出新的全变差最小化目标函数,通过将上一步迭代重建的图像作为反馈加入到新的迭代之中,不断更新目标函数的已知项。在算法求解时,采用增广Lagrangian罚函数方法,将约束问题非约束化,并将之转化为等价的3个子问题,通过在交替方向上求解子问题来获得优化问题的最优解。实验结果表明,该算法重建出的图像信息完整,细节清晰,重建精度高,与Split Bregman算法相比,本文算法结果的相对均方误差可下降42.1%~98.5%,条纹指标可下降42.8%~98.5%。 相似文献
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《中国航空学报》2021,34(4):332-340
Bionic adhesives with tip-expanded microstructural arrays have attracted considerable interest owing to their high adhesive performance at low preloads. Their mainstream manufacturing method is molding. Due to most molds are made of silicon or silicon-based soft templates, and have poor wear resistant or vulnerability to high temperature, limiting their use in large-scale manufacturing. Nickel is widely used as an embossing mold in the micro/nano-imprint industrial process owing to its good mechanical properties. However, the processing of metal molds for the fabrication of tip-expanded microstructural arrays is extremely challenging. In this study, using electrodeposition techniques, the shape of the micropores is modified to obtain end-controlled pores. The effect of the non-uniformity of the electric field on the microporous morphology in the electrodeposition process is systematically investigated. Furthermore, the mechanism of non-uniformity evolution of the microporous morphology is revealed. The optimized microporous metal array is used as a mold to investigate the cavity evolution laws of the elastic cushions under pre-load during the manufacturing process. As a result, typical bionic adhesives with tip-expansion are obtained. Moreover, corresponding adhesion mechanics are analyzed. The results show that electrochemical modifications have broad application prospects in the fabrication of tip-expanded microstructures, providing a new method for the large-scale fabrication of bionic adhesives based on metal molds. 相似文献