Corrosion fatigue behavior of fastening hole structure and virtual crack propagation tests

Journal of University of Science and Technology Beijing: Mineral Metallurgy Materials (Eng Ed)

Volumn 15, Issue 5, 2008, Pages 585-589

  Zhang, Youhong ^a,b   Chang, Xinlong ^a   Lv, Guozhi ^b   Wang, Hui ^b   Li, Zhong ^b   Cheng, Yueliang ^c  

^a ROCKET FORCE UNIVERSITY OF ENGINEERING   (China)

^b NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

^c NAVAL AERONAUTICAL AND ASTRONAUTICAL UNIVERSITY   (China)

Author keywords

AFGROW; aluminum alloy; corrosion fatigue; crack propagation; stochastic process

Indexed keywords

ALLOYS; ALUMINA; ALUMINUM; ALUMINUM ALLOYS; CORROSION; CRACK DETECTION; CRACK PROPAGATION; CRACKING (CHEMICAL); CRACKS; EXPERIMENTS; FATIGUE CRACK PROPAGATION; FATIGUE OF MATERIALS; GROWTH (MATERIALS); LIGHT METALS; PROBABILITY DISTRIBUTIONS; SODIUM CHLORIDE; STOCHASTIC MODELS; SYSTEMS ENGINEERING; VIRTUAL REALITY;

3.5 WT% NACL SOLUTIONS; AFGROW; CORROSION FATIGUE CRACK GROWTHS; CORROSIVE ENVIRONMENTS; CRACK GROWTH CURVES; CRACK GROWTH RATES; CRACK LENGTH DISTRIBUTIONS; CRACK SIZES; FATIGUE CRACK PROPAGATION BEHAVIORS; HOLE STRUCTURES; LOADING FREQUENCIES; LOG NORMAL PROCESSES; LY12CZ ALUMINUM ALLOYS; NUMBER OF CYCLES; PARIS EQUATIONS; PROBABILISTIC MODELS; SIMULATION METHODS; STOCHASTIC PROCESS; VIRTUAL CRACKS; VIRTUAL SIMULATIONS;

CORROSION FATIGUE;

EID: 58149177307     PISSN: 10058850     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1005-8850(08)60109-7     Document Type: Article

References (10)

1. Y.L. Chen, The Effect of Corrosion to the Residual Strength of the Served Aircraft Structure [Dissertation] (in Chinese), Northwest Polytechnical University, Xi'an, 2004, p.10.
2. Bellinger N.C., and Komorowski J.P. Corrosion pillowing stresses in fuselage lap joints. AIAA J. 35 2 (1997) 317
3. P. Shi, Corrosion Fatigue Reliability of Aging Structures [Dissertation], Lehigh University, 2002, p.50.
4. Wu W.F., and Ni C.C. A study of stochastic fatigue crack growth modeling through experimental data. Probab. Eng. Mech. 18 1 (2003) 107
5. Maymon G. The problematic nature of the application of stochastic crack growth models in engineering design. Eng. Fract. Mech 53 6 (1996) 911
6. Maymon G. Probabilistic crack growth behavior of aluminum 2024-T351 alloy using the 'unified' approach. Int. J. Fatigue 27 6 (2005) 828
7. Y.H. Zhang, The Corrosion Damage and its Effect to the Life of Aircraft Structure [Dissertation] (in Chinese), Northwest Polytechnical University, Xi'an, 2007, p.88.
8. Yang J.N., and Manning S.D. A simple second order approximation for stochastic crack growth analysis. Eng. Fract. Mech. 53 3 (1996) 678
9. Harter J.A. AFGROW Users Guide and Technical Manual (2002), AFRL-VA-WP-TR-2002, Air Force Research Laboratory, USA 28
10. Bellinger N.C., Komorowski J.P., and Benak T.J. Residual life predictions of corroded fuselage lap joints. Int. J. Fatigue 23 Suppl. (2001) 354