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Accurate stress intensity factor solutions for corner cracks at a hole

机译:孔角裂纹的精确应力强度因子解决方案

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Laboratory test and in-service experience shows fatigue cracks at holes exhibit unsymmetric growth; thus, the need for the new solutions is paramount. Stress intensity factor, K, solutions for symmetric and unsymmetric corner cracks at a hole subject to general loading were determined using a hp-version of the finite element method (FEM) in conjunction with a mathematical splitting scheme to enable efficient, accurate calculations. In traditional applications of the FEM, mesh generation is labor intensive; however, using the splitting scheme, stress intensity functions are obtained without explicitly including the crack in the FE mesh of the global structure. By using the hp-version of FEM, a set of K-solutions converging exponentially fast to the exact solution is obtained. The crack is analyzed in the local domain with easily generated FE meshes. All structurally significant crack shapes were considered; specifically, crack depth to crack length ratios (a/c) of 0.1-10.0, crack depth to sheet thickness ratios (a/t) of 0.100.99, and hole radius to sheet thickness ratios (r/t) = 1.0. The loading conditions were remote tension, remote bending, and pin loading (bearing). In addition, all combinations of a/c and a/t are analyzed at each side of the hole; thus 226,875 solutions were developed with control of the error in the computed K solutions. Calculated relative error is generally much smaller than 1 percent along the entire crack front including the vertex regions. Comparisons are made to solutions in the open literature. The new K solutions show the literature solutions are, in general, accurate for all three load conditions; however, for the extreme cases of a/c, a/t, and r/t; the literature solutions differ by as much as 26 percent.
机译:实验室测试和使用经验表明,孔处的疲劳裂纹表现出不对称的增长;因此,对新解决方案的需求至关重要。使用有限元方法(FEM)的hp版本并结合数学拆分方案来确定有效载荷下孔中对称和非对称角部裂纹的应力强度因子K和解,以实现高效,准确的计算。在FEM的传统应用中,网格生成是劳动密集型的。但是,使用分裂方案时,无需在整体结构的有限元网格中明确包含裂纹即可获得应力强度函数。通过使用hp版本的FEM,可以获得一组K指数解,快速收敛到精确解。使用易于生成的有限元网格在局部区域分析裂纹。考虑了所有结构上显着的裂纹形状;具体地说,裂纹深度与裂纹长度之比(a / c)为0.1-10.0,裂纹深度与薄片厚度之比(a / t)为0.100.99,孔半径与薄片厚度之比(r / t)= 1.0。加载条件为远程张力,远程弯曲和销加载(轴承)。另外,在孔的每一侧都分析了a / c和a / t的所有组合。因此,通过控制所计算的K个解中的误差,开发了226,875个解。在包括顶点区域在内的整个裂纹前沿,计算得出的相对误差通常都小于1%。比较开放文献中的解决方案。新的K解表明,文献中的解决方案通常对于所有三种负载情况都是准确的。但是,在极端情况下,例如a / c,a / t和r / t;文献中的解决方案相差高达26%。

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