Abstract
The stress intensity factorK in the tip of crack which is in the corner of the frame component has been calculated indirectly by means of numeric calculation ofJ Integral. Some laws and relationships among the stress intensity factorK, the applied loads and the crack length for this kind of components have been discovered for the first time. The calculating formula forK has been deduced, the criticalK has been calculated with the formula, that is 5 811.56–6 122.58 MPa · mm1/2. The conclusions reached in this paper are of great referential and practical value for simplifying the calculation of stress intensity factorK for this type of components.
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References
The Chinese Research Institute of Aviation. Handbook of stress intensity factor (in Chinese). Beijing: Science Technology Press, 1981. 11–52
Zhang Hang. The calculating methods of stress intensity factor in fracture mechanics (in Chinese). Beijing: National Defence Industry Press, 1992. 80–179
Rice J R. A path indepadent integral and the approxinate analysis of strain concentrations by notches and cracks. Journal of Applied Mechanics, 1968, 35(2): 379–386
Wang Lunfu. Theory of elastic (in Chinese). Beijing: Science Technology Press, 1979. 72–74
Ying Shangzhen. Theory of fracture and damage and its application (in Chinese). Beijing: Qinghua Press, 1992. 115–119
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Project supported by Technological Development Foundation of the Nonferrous Metal Industry Corporation of China
Synopsis of the first author Liu Yilun, Doctor, associate professor, born in Oct. 30, 1955. Research areas are fatigue strength of component and the technology of continuous casting for non-ferrous metal.
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Liu, Y., Wang, A. & He, M. On the calculation of stress intensity factorK for frame components. J. Cent. South Univ. Technol. 2, 37–41 (1995). https://doi.org/10.1007/BF02652005
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DOI: https://doi.org/10.1007/BF02652005