Abstract
An engineering calculation method of predicting probability distribution for crack initiation life of structures susceptible to widespread fatigue damage is proposed. Through a study of the crack initiation mechanism, the incident that crack initiation life of multiple detail structure taking a certain value is transformed into the intersection of three independent incidents. The probability of occurrence of the former incident is the product of the probability of occurrence of the latter three independent incidents, which is derived from the probability distribution function of crack initiation life of single detail structure. Thus, the detailed formulae of probability density functions of initiation lives for cracks appearing in turn in multiple detail structure are obtained. Making use of these detailed formulae, the calculation formula of median rank of initiation life is derived. It is only related to failure order and total number of details. Through the value of median rank, the initiation life with reliability of 50% can be achieved. Thus, an engineering calculation formula of probability distribution of crack initiation life is gotten. Crack initiation test of specimens with a single hole and multiple holes were carried out. The model is used to estimate crack initiation lives of the multiple holes notched specimens. The predicted results are in good agreement with the testing results, which show that this model is effective.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Federal Aviation Administration: Aging airplane program: widespread fatigue damage; final rule. Amendment Nos. 25–132, 26–5, 121–351, 129–48, Docket No. FAA-2006-24281; Federal Register, Vol. 75, No. 219 (2010)
Gao, Z.T., Xiong, J.J.: Fatigue Reliability. Beijing: Beijing University of Aeronautics and Astronautics Press, pp. 74–76 (in Chinese) (2000)
Li, Z.N., Guan, Z.D., Zhang, J.K., Wang, J., He, X.F.: Applied Fracture Mechanics. Beijing: Beijing University of Aeronautics and Astronautics Press, pp. 191–192 (in Chinese) (2012)
Nelson, W.: Applied Life Data Analysis. Wiley, New York (1982)
Pidaparti, R.M.V., Palakal, M.J., Rahman, Z.A.: Simulation of structural integrity predictions for panels with multiple site damage. Adv. Eng. Softw. 31(2), 127–135 (2000)
Pieracci A, Mengali G.: An assessment of multiple site damage through a simple statistical model. In: AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, 40th, AIAA/ASME/AHS Adaptive Structures Forum and AIAA Forum on Non-Deterministic Approaches, pp. 1993–2002. AIAA, St. Louis, MO (1999)
Pitt, S., Jones, R.: Multiple-site and widespread fatigue damage in aging aircraft. Eng. Fail. Anal. 4(4), 237–257 (1997)
Proppe, C.: Probabilistic analysis of multi-site damage in aircraft fuselages. Comput. Mech. 30(4), 323–329 (2003)
Silva, L.F.M., Gonçalves, J.P.M., Oliveira, F.M.F., Castro, P.M.S.T.: Multiple-site damage in riveted lap-joints: experimental simulation and finite element prediction. Int. J. Fatigue 22(4), 319–338 (2000)
Wang, S., Liu, M.b., Wang, G.L., Wang, X.B.: Test research and finite element analysis on multiple site damage. Acta Aeronaut. Astronaut. Sin. 31(8), 1578–1583 (in Chinese) (2010)
Xue, J.C., Gong, Y.Z.: The probability model to preestimate onset of initial widespread fatigue damage. In: The 18th National Academic Conference on Structural Engineering, pp. 597–600. Guangzhou (in Chinese) (2009)
Zhang, J.Y., Bao, R., Zhang, X., Fei, B.J.: A probabilistic estimation method of multiple site damage occurrence for aircraft structures. Procedia Eng. 2(1), 1115–1124 (2010)
Zheng, X.L.: Durability and Damage Tolerance Design Manual for Civil Aircraft Structure. Beijing: Aviation Industry Press, pp. 334–335 (in Chinese) (2003)
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2020 Springer Nature Switzerland AG
About this paper
Cite this paper
Wei, X., Qiang, L., Peiliang, S., Gang, Y., Fu, H., Jianjun, Z. (2020). An Engineering Calculation Method of Probability Distribution of Crack Initiation Life for Widespread Fatigue Damage. In: Niepokolczycki, A., Komorowski, J. (eds) ICAF 2019 – Structural Integrity in the Age of Additive Manufacturing. ICAF 2019. Lecture Notes in Mechanical Engineering. Springer, Cham. https://doi.org/10.1007/978-3-030-21503-3_29
Download citation
DOI: https://doi.org/10.1007/978-3-030-21503-3_29
Published:
Publisher Name: Springer, Cham
Print ISBN: 978-3-030-21502-6
Online ISBN: 978-3-030-21503-3
eBook Packages: EngineeringEngineering (R0)