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A single edge notch specimen for fatigue, creep-fatigue and thermo-mechanical fatigue crack growth testing

机译:用于疲劳,蠕变 - 疲劳和热机械疲劳裂纹生长试验的单个边缘凹口标本

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The importance of capturing crack growth behavior under creep-fatigue and thermo-mechanical-fatigue is well known. Such service load environments are often simulated by performing tests under load and displacement control conditions where the specimen may be subjected to both tensile and compressive loads. A single edge notch specimen was developed to accommodate tension and compression loading in fatigue, creep-fatigue and thermo-mechanical fatigue crack growth experiments. The stress intensity factor and compliance solutions were developed for the single edge notch specimen using a 3D fracture code (FRANC3D) and 2D boundary element code (FADD2D). Both codes agreed well with each other. It is shown in this work that using simple approximations in a 2D code such as FADD2D, accurate stress-intensity and compliance solutions can be obtained for specimen geometry with varying cross sections. An importance of using correct boundary condition is emphasized by displaying the difference in stress intensity solutions for rectangular edge-cracked plate under uniform-stress, and uniform-displacement cases. Also, it is shown that stress intensity solution for a threaded edge-cracked specimen considered in this paper is different from the solution for rectangular edge-cracked plate under displacement control. Asa validation of the developed stress-intensity and compliance equations, fatigue crack growth tests were conducted using the single edge notch, compact type and a surface crack specimen. Tests were conducted under constant amplitude load control of 0.1 stress ratio,Rfor IN738 nickel base super alloy material. Agreement was found between the different specimen types in the intermediate crack growth rate range.
机译:捕获蠕变疲劳和热机械疲劳下捕获裂纹生长行为的重要性是众所周知的。这种服务负荷环境通常通过在负载和位移控制条件下进行测试而模拟,其中样品可以经受拉伸和压缩载荷。开发了一个边缘凹口标本以适应疲劳,蠕变 - 疲劳和热机械疲劳裂纹生长实验的张力和压缩负荷。使用3D骨折码(FRANC3D)和2D边界元件代码(FADD2D)为单边缘凹口标本开发应力强度因子和合规解决方案。两项代码彼此一致。在这项工作中示出,可以使用诸如FADD2D,精确的应力强度和合规性解决方案中的2D代码中的简单近似,以获得具有不同横截面的试样几何形状。通过在均匀应力下显示矩形边缘破裂板的应力强度溶液和均匀 - 位移壳体来强调使用使用正确边界条件的重要性。此外,示出了本文考虑的螺纹边缘破裂样本的应力强度溶液与位移控制下的矩形边缘破裂板的溶液不同。 ASA验证发育的应力强度和柔性方程,使用单边缘凹口,紧凑型和表面裂纹标本进行疲劳裂纹生长试验。在0.1应力比的恒定幅度负荷控制下进行测试,镍氢镍基镍基超合金材料。在中间裂纹增长速率范围内不同标本类型发现协议。

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