Fatigue Crack Growth of Aircraft Aluminum Alloys

作者: Sp. G. Pantelakis , Al Th. Kermanidis

DOI: 10.1007/978-1-4020-8520-8_13

关键词: Crack closureFatigue testingComposite materialParis' lawAluminiumMaterials scienceFatigue crack propagation

摘要:

参考文章(20)
S. Suresh, Fatigue of materials ,(1991)
GH Bray, RJ Bucci, EL Colvin, M Kulak, Effect of Prior Corrosion on the S/N Fatigue Performance of Aluminum Sheet Alloys 2024-T3 and 2524-T3 ASTM special technical publications. pp. 89- 103 ,(1997) , 10.1520/STP19955S
G. N. Haidemenopoulos, N. Hassiotis, G. Papapolymerou, V. Bontozoglou, Hydrogen absorption into aluminum alloy 2024-T3 during exfoliation and alternate immersion testing Corrosion. ,vol. 54, pp. 73- 78 ,(1998) , 10.5006/1.3284830
O. D. Smiyan, M. V. Koval', R. K. Melekhov, N. L. Korobanova, A. M. Krutsan, V. A. Yakovchik, Local corrosion damage of aluminum alloys Materials Science. ,vol. 19, pp. 422- 426 ,(1984) , 10.1007/BF00721534
P.S. Pao, L.A. Cooley, M.A. Imam, G.R. Yoder, Fatigue-crack growth in 2090 AlLi alloy Scripta Metallurgica. ,vol. 23, pp. 1455- 1460 ,(1989) , 10.1016/0036-9748(89)90076-8
E. Zaiken, R.O. Ritchie, On the location of crack closure and the threshold condition for fatigue crack growth Scripta Metallurgica. ,vol. 18, pp. 847- 850 ,(1984) , 10.1016/0036-9748(84)90408-3
G.G Garrett, J.F Knott, Crystallographic fatigue crack growth in aluminium alloys Acta Metallurgica. ,vol. 23, pp. 841- 848 ,(1975) , 10.1016/0001-6160(75)90200-X
Al.Th. Kermanidis, P.V. Petroyiannis, Sp.G. Pantelakis, Fatigue and damage tolerance behaviour of corroded 2024 T351 aircraft aluminum alloy Theoretical and Applied Fracture Mechanics. ,vol. 43, pp. 121- 132 ,(2005) , 10.1016/J.TAFMEC.2004.12.008
Sp.G. Pantelakis, P.G. Daglaras, Ch.Alk. Apostolopoulos, Tensile and energy density properties of 2024, 6013, 8090 and 2091 aircraft aluminum alloy after corrosion exposure Theoretical and Applied Fracture Mechanics. ,vol. 33, pp. 117- 134 ,(2000) , 10.1016/S0167-8442(00)00007-0