[1]Budnick J.NAVAIR air vehicle corrosion challenges[C]. Tri-Service Corrosion Conference. Las Vegas: US Department of Defence, 2003.[2]张有宏, 吕国志, 陈跃良.铝合金预腐蚀及疲劳损伤研究[J].航空学报, 2005, 26(6):779-782[3]Petroyiannis PV, Kermanidis AT, Akid R, Rodopoulos CA, Pantelakis SG.Analysis of the effects of exfoliation corrosion on the fatigue behaviour of the 2024-T351 aluminium alloy using the Fatigue Damage Map[J].International Journal of Fatigue, 2005, 27(7):817-827[4]谭晓明, 张丹峰, 卞贵学, 等.腐蚀对新型高强度铝合金疲劳裂纹萌生机制及扩展行为的作用[J].机械工程学报, 2014, 50(22):76-83[5]Bray GH, Bucci RJ, Colvin EL, Kulak M.Effect of prior corrosion on the S/N fatigue performance of aluminum sheet alloys 2024-T3 and 2524-T3[J]. ASTM special technical publication, 1997, 1298: 89-103.[J].ASTM special technical publication, 1997, 1298(5):89-103[6]May ME, Luc TP, Saintier N, Devos O.Effect of corrosion on the high cycle fatigue strength of martensitic stainless steel X12CrNiMoV12-3[J].International Journal of Fatigue, 2013, 47(2):330-339[7]Kermanidis AT, Petroyiannis PV, Pantelakis.Fatigue and damage tolerance behavior of corroded 2024 T351 aircraft aluminum alloy[J].Theory and Applied Fracture Mechanics, 2005, 43(1):121-132[8]Aydin M, Savaskan T.Fatigue properties of zinc-aluminum alloys in 35% NaCl and 1% Hcl solutions[J].International Journal of Fatigue, 2004, 26(1):103-110[9]Wang SQ, Zhang DK, Chen K, Xu LM, Ge SR.Corrosion fatigue behaviors of steel wires used in coalmine[J].Materials and Design, 2014, 53(1):58-64[10]Wang QY, Pidaparti RM, Palakal MJ.Comparative study of corrosion-fatigue in aircraft materials[J].American Institute of Aeronautics and Astronautics, 2001, 39(2):325-330[11]Ishihara S, Saka S, Nan ZY, Goshima T, Sunada S.Prediction of corrosion fatigue lives of aluminum alloy on the basis of corrosion pit growth law[J].Fatigue Fracture& Engineering of Materials& Structure, 2006, 29(6):472-480[12]Sriaman MR, Pidapati RA.Life prediction of aircraft aluminum subjected to pitting corrosion under fatigue condition[J].Journal of Aircraft, 2009, 46(4):1253-1259[13]Ghidini T,Donne CD.Fatigue life predictions using fracture mechanics methods[J].Enginnering Fracture Mechanics, 2009, 76(1):134-148[14]Codaro EN, Nakazato RZ, Horovistiz AL, Ribeiro LMF, Ribeiro RB, Hein LRO.An image processing method for morphological characterization and pitting corrosion evaluation[J].Material Science and Engineering. A, 2002, 334(1-2):298-306[15]Ghali E, Dietzel W, Kainer KU.Testing of general and localized corrosion of magnesium alloys: A critical review[J].Journal of Materials Engineering and Performance, 2004, 13(5):7-23[16]Li SX, Akid R.Corrosion fatigue life prediction of a steel shaft material in seawater[J].Engineering Failure Analysis, 2013, 34(8):324-334[17]Shekhter A, Loader C, Hu W.Assessment of the Effect of Pitting Corrosion on the Safe Life Prediction of the P-3C[R]. DSTO-TR-2080, Victoria Australia: Air Vehicles Division Defence Science and Technology Organisation (DSTO), 2007.[18]Mills T, Sharp PK, Loader C.The Incorporation of Pitting Corrosion Damage into F-111 Fatigue Life Modeling[R]. DSTO-RR-0237, Victoria Australia: Air Vehicles Division Defence Science and Technology Organization, 2002.[19]Sharp P K, Barter S A, Clark G.Localized Life Extension Specification for the F/A-18 Y470 X19 Pocket[R]. DSTO-TN-0279, Victoria Australia: Air Vehicles Division Defence Science and Technology Organisation(DSTO), 2000.[20]American Society for Testing Materials International.Standard test method for exfoliation corrosion susceptibility in 2XXX and7XXX series aluminum alloys: ASTM G34-01[S]. West Conshohocken, PA: American Society for Testing and Materials International, 2007: 2-7.[21]Walde K, Brockenbroughb JR, Craigc BA, Hillberry BM.Multiple fatigue crack growth in pre-corroded 2024-T3 aluminum[J].International Journal of Fatigue, 2005, 27(10-12):1509-1518[22]Walde K, Hillberry BM.Characterization of pitting damage and prediction of remaining fatigue life[J].International Journal of Fatigue, 2008, 30(1):106-118[23]Nan ZY, Ishihara S, Goshima T.Corrosion fatigue behavior of extruded magnesium alloy AZ31 in sodium chloride solution[J].International Journal of Fatigue, 2008, 30(7):1181-1188[24]Medved JJ, Breton M, Irving PE.Corrosion pit size distributions and fatigue lives-a study ofthe EIFS technique for fatigue design in the presence of corrosion[J].International Journal of Fatigue, 2004, 26(1):71-80[25]Chaussumier M, Mabru C, Shahzad M, Chieragatti R, Aria FR.A predictive fatigue life model for anodized 7050 aluminium alloy[J].International Journal of Fatigue, 2013, 48(1):205-213[26]Green AE, Sneddon IN.The stress distribution in the neighborhood of a flat elliptic crack in an elastic solid[J].Proceedings of the Royal Society A, 1946, 187(1009):229-260[27]Irwin G R.Crack extension force for a part-through crack in a plate[J].Journal of Applied mechanics, 1962, 29(4):651-654[28]中国航空研究院.应力强度因子手册[M]. 北京:科学出版社,1993.[29] Xiong JJ, Shenoi RA.Fatigue and fracture reliability engineering[M]. London: Springer, 2011[30]北京航空材料研究所.航空金属材料疲劳裂纹扩展速率手册[M]. 北京:北京航空材料研究所,1984. |