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ACCURATE CRITICAL STRESS INTENSITY FACTOR GRIFFITH CRACK THEORY MEASUREMENTS BY NUMERICAL TECHNIQUES

机译:精确的临界应力强度因子Griffith裂纹理论测量的数值方法

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Critical stress intensity factor (K_(Ic)) has been an approximation for fracture toughness using only load-cell measurements. However, artificial man-made cracks several orders of magnitude longer and wider than natural flaws have required a correction factor term (Y) that can be up to about 3 times the recorded experimental value [1-3]. In fact, over 30 years ago a National Academy of Sciences advisory board stated that empiricalK_(Ic) testing was of serious concern and further requested that an accurate bulk fracture toughness method be found [4]. Now that fracture toughness can be calculated accurately by numerical integration from the load/deflection curve as resilience, work of fracture (WOF) and strain energy release (S_(Ic)) [5, 6], K_(Ic) appears to be unnecessary. However, the large body of previous K_(Ic) experimental test results found in the literature offer the opportunity for continued meta analysis with other more practical and accurate fracture toughness results using energy methods and numerical integration. Therefore, K_(Ic) is derived from the classical Griffith Crack Theory [6] to include S_(Ic) as a more accurate term for strain energy release rate (G_(Ic)), along with crack surface energy (γ), crack length (a), modulus (E), applied stress (σ), Y, crack-tip plastic zone defect region (rp) and yield strength (oys) that can all be determined from load and deflection data. Polymer matrix discontinuous quartz fiber-reinforced composites to accentuate toughness differences were prepared for flexural mechanical testing comprising of 3 mm fibers at different volume percentages from 0-54.0 vol% and at 28.2 vol% with different fiber lengths from 0.0-6.0 mm. Results provided a new correction factor and regression analyses between several numerical integration fracture toughness test methods to support K_(Ic) results. Further, bulk K_(Ic) accurate experimental values are compared with empirical test results found in literature. Also, several fracture toughness mechanisms are discussed especially for fiber-reinforced composites.
机译:临界应力强度因子(K_(Ic))是仅使用测力传感器测量得出的断裂韧性的近似值。然而,人造裂缝比自然裂缝要长和宽几个数量级,因此需要的校正因子项(Y)最高可达记录的实验值的三倍[1-3]。实际上,在30年前,美国国家科学院顾问委员会表示,经验K_(Ic)测试受到严重关注,并进一步要求找到一种准确的整体断裂韧性方法[4]。现在,可以通过载荷/挠度曲线的数值积分来精确计算断裂韧性,因为回弹力,断裂功(WOF)和应变能释放(S_(Ic))[5,6]似乎不需要K_(Ic) 。然而,文献中发现的大量先前的K_(Ic)实验测试结果为通过使用能量方法和数值积分的其他更实用,准确的断裂韧性结果提供了继续进行meta分析的机会。因此,K_(Ic)源自经典的格里菲斯裂纹理论[6],其中包括S_(Ic)作为应变能释放率(G_(Ic))的更准确术语,以及裂纹表面能(γ),裂纹长度(a),模量(E),施加应力(σ),Y,裂纹尖端塑性区缺陷区域(rp)和屈服强度(oys)都可以根据载荷和挠度数据确定。制备了用于增强弯曲强度差异的聚合物基体不连续石英纤维增强复合材料,用于挠曲机械测试,该测试包括3mm纤维,其体积百分比为0-54.0%(体积百分比)和28.2vol%,纤维长度为0.0-6.0mm。结果提供了一种新的校正因子,并在几种数值积分断裂韧性测试方法之间进行了回归分析,以支持K_(Ic)结果。此外,将大量的K_(Ic)准确的实验值与文献中的经验测试结果进行了比较。此外,讨论了几种断裂韧性机制,尤其是对于纤维增强复合材料。

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