Fatigue damage analysis of wing-fuselage attachment lug
Tài liệu tham khảo
Antoni, 2011, Analytical Modelling for Static Stress Analysis of Pin-Loaded Lugs with Bush Fitting, Applied Mathematical Modelling, 35, 1, 10.1016/j.apm.2010.05.002
Atluri, S.N., Nishioka, T., 1986. Computational Methods for Three-Dimensional Problems of Fracture, in “Computational Methods in Mechanics of Fracture”. In: Atluri, S.N. (Ed.), pp. 230-287.
Barsoum, 1977, Triangular Quarter-Point Elements as Elastic and Perfectly-Plastic Crack Tip Elements, International Journal for Numerical Methods in Engineering, 11, 85, 10.1002/nme.1620110109
Bodner, 1983, A Description of Fatigue Crack Growth in Terms of Plastic Work, Engineering Fracture Mechanics, 17, 189, 10.1016/0013-7944(83)90169-8
Boljanović, 2014, Fatigue Crack Growth Modeling of Attachment Lugs, International Journal of Fatigue, 58, 66, 10.1016/j.ijfatigue.2013.03.016
Elber, 1971, The Significance of Fatigue Crack Closure, in “Damage Tolerance in Aircraft Structure”, ASTM STR 486, Philadelphia, American Society for Testing and Materials, 230
Geier, W., 1980. Strength Behaviour of Fatigue Cracked Lugs. Royal Aircraft Establishment, LT 20057.
Hsu, 1981, Analysis of Cracks at Attachment Lugs, Journal of Aircraft, 18, 755, 10.2514/3.57558
Huang, 2007, Improved Modeling of the Effect of R-Ratio on Crack Growth rate, International Journal of Fatigue, 29, 591, 10.1016/j.ijfatigue.2006.07.014
Kathiresan, K., Brussat, T.R., 1984. Advanced Life Analysis Methods, AFWAL-TR-84-3080, Ohio, USA.
Kujawski, 2001, A New (∆K + Kmax) 0.5 Driving Force Parameter for Crack Growth in Aluminum Alloy, International Journal of Fatigue, 23, 733, 10.1016/S0142-1123(01)00023-8
Mikheevskiy, 2012, Analysis of Fatigue Crack Growth in an Attachment Lug Based on the Weight Function Technique and the UniGrow Fatigue Crack Growth Model, International Journal of Applied Fatigue, 42, 88, 10.1016/j.ijfatigue.2011.07.006
Nicholls, 1994, Prediction of Fatigue Crack Growth Rates Based on Crack Blunting, Engineering Fracture Mechanics, 48, 9, 10.1016/0013-7944(94)90138-4
Rigby, 1997, Stress Intensity Factors for Cracks at Attachment Lugs, Engineering Failure Analysis, 4, 133, 10.1016/S1350-6307(97)00004-6
Wu, 2011, Study on Fatigue Crack Growth Model of Attachment Lug Subjected to Oblique Pin-Load, Advanced Materials Research, 291-294, 1043, 10.4028/www.scientific.net/AMR.291-294.1043