13th International Conference on Fracture June 16–21, 2013, Beijing, China -10- [3] Kirkby, W. T., and Rooke, D. P.. A Fracture Mechanics Study of Residual Strength of Pin-Lug Specimens. Frac. Mech. in Eng. Practice. 1977: 339. [4] Cartwright, D. J., and Rooke, D. P.. Approximate Stress Intensity Factors Compounded from Known Solutions. Eng. Frac. Mech. 1974;6:563-571. [5] Schijve, J., and Hoeymakers, A.H.W.. Fatigue Crack Growth in Lugs and the Stress Intensity Factor. Report LR-273, Delft University of Technology, Delft, the Netherlands, July 1978. [6] Wanhill, R.J.H., and Lof, C.F.. Calculation of Stress Intensity Factors for Corner Cracking in a Lug. Frac. Mech. Design Methodology. ARGARD CP221, February 1977, Paper No. 8. [7] James, L. A., and Anderson, W. E.. A Simple Experimental Procedure for Stress Intensity Factor Calibration. Eng. Frac. Mech. 1969;1:565-568. [8] Pian, T. H. H., Mar, J. W., Orringer, O., and Stalk, G.. Numerical Computation of Stress Intensity Factors for Aircraft Structural Details by the Finite Element Method. AFFDL-TR-76-12, Air Force Flight Dynamics Laboratory, May 1976. [9] Aberson, J. A., Anderson, J. M.. Cracked Finite-Elements Proposed for NASTRAN. Third NASTRAN Users’ Colloquium, NASA TMX-2893, 1973:531-550. [10]Impellizzeri, L. F., and Rich, D. L.. Spectrum Fatigue Crack Growth in Lugs. Fatigue Crack Growth Under Spectrum Loads, ASTM STP 595, 1976:320-336. [11] Bueckner, H. F.. Weight Functions for the Notched Bar. Zeitschrift for Angewandte Mathematik und Mechanik. 1971;51: 97-109. [12]Jong-Ho Kim, Soon-Bok Lee, Seong-Gu Hong. Fatigue crack growth behavior of Al7075-T7451 attachment lugs under flight spectrum variation. Eng. Fract. Mech. 2003;40:135-144. [13]S.Baster, L. Molent, N.Goldsmith, R.Jones. An experimental evaluation of fatigue crack growth. Eng. Fail. Anal. 2005;12:99-128. [14]Xue Jingchuan. Bolt and Lug Strength Analysis Handbook. Beijing: Aviation Industry Press;1998. [15]Zheng Xiaoling. Civil Aircraft Durability and Damage Tolerance Design Handbook. Beijing: Aviation Industry Press;2003. [16] Interpreted by Scientific and Technical Research Institute of Ministry of Aero-space Industry. USAF Damage Tolerance Design Handbook. Xi’an: Northwest Polytechnical University Press;1989.
RkJQdWJsaXNoZXIy MjM0NDE=