Fatigue life prediction under random loading conditions in 7475-T7351 aluminum alloy using the RMS model

International Journal of Damage Mechanics

Volumn 15, Issue 1, 2006, Pages 89-102

  Kim, Sang Tae ^a   Tadjiev, Damir ^a   Yang, Hyun Tae ^a  

^a Yeungnam University   (South Korea)

Author keywords

7475 T7351 aluminum alloy; Fatigue crack growth prediction under random loading; Fatigue of materials; RMS model

Indexed keywords

ALUMINUM ALLOYS; CRACK PROPAGATION; FATIGUE TESTING; MATHEMATICAL MODELS; STRESS INTENSITY FACTORS;

FATIGUE LIFE PREDICTION; RANDOM LOADING; ROOT MEAN SQUARE (RMS) MODEL;

FATIGUE OF MATERIALS;

EID: 31544459229     PISSN: 10567895     EISSN: 15307921     Source Type: Journal    
DOI: 10.1177/1056789506058605     Document Type: Article

References (21)

1. Advanced Damage Analysis Modular System (ADAMSys), Lockheed Fort Worth Company, USA.
2. Chang/Hudson (1981). Methods and Models for Predicting Fatigue Crack Growth under Random Loading, ASTM STP 748.
3. Christensen, R.H. (1959). Fatigue Crack, Fatigue Damage and their Detection, J. Metal Fatigue, McGraw-Hill, New York.
4. Forman, R.G., Kearney, V.E. and Engle, R.M. (1967). Transactions of the American Society of Mechanical Engineers. Series D; Journal of Basic Engineering, 89(3): 459-465, Sept.
5. Hudson, C.M. and Hardrath, H.F. (1963). Investigation of the Effects of Variable Amplitude Loadings on Fatigue Crack Propagation Patterns, TND-1803, NASA.
6. Hudson, C.M. (1982). A Root-Mean-Square Approach for Predicting Fatigue Crack Growth under Random Loading, In: Chang, J.B. and Hudson, C.M. (eds), Methods and Models for Predicting Fatigue Crack Growth under Random Loading, ASTM STP 748, pp. 41-52.
7. Johnson, W.S. (1981). Multi-Parameter Yield Zone Model for Predicting Spectrum Crack Growth, In: Chang, J.B. and Hudson, C.M. (eds), Methods and Models for Predicting Fatigue Crack Growth under Random Loading, ASTM STP 748, pp. 85-102.
8. Lang (2000). A Model for Fatigue Crack Growth - Part II: Modeling, J. Fatigue Fracture of Engineering Materials and Structures, 23(7): 603-617.
9. Moreno, B., Zapatero, J. and Dominguez, J. (2003). An Experimental Analysis of Fatigue Crack Growth under Random Loading, International Journal of Fatigue, 25(8): 597-608.
10. Narayanaswami, R. (2001). Fatigue Crack Growth in Selected Aluminium Alloys under Variable Amplitude Loading, In: Proceedings of the VII Summer School of Fracture Mechanics, Pokrzywna (Poland), pp. 317-333.
11. Newman, Jr., J.C. (1973). Engineering Fracture Mechanics, Vol. 5, #3, pp. 667-689.
12. Newman, Jr., J.C. (1997). Prediction of Crack Growth under Variable-Amplitude Loading in Thin-Sheet 2024-T3 Aluminium Alloys, Engineering Against Fatigue, University of Sheffield, NASA Langley Research Center, Hampton, Virginia, USA.
13. Newman, Jr., J.C. (1982). Prediction of Fatigue Crack Growth under Variable-Amplitude and Spectrum Loading Using a Closure Model, Design of Fatigue and Fracture Resistant Structures, ASTM STP 761, pp. 255-277.
14. Rolfe, S.T. and Barsom, J.M. (1975). Fracture and Fatigue Control in Structures, Prentice Hall Inc., Englewood Cliffs, NJ, pp. 272-291.
15. Schijve, J. and Broek, D. (1962). The Result of a Test Program based on a Gust Spectrum with Variable Amplitude Loading, Aircraft Engineering, 34: 314-316.
16. Schijve, J. (1972). The Accumulation of Fatigue Damage in Aircraft Materials and Structures, AGAR Dograph 157.
17. Skopura, M. (1996). Empirical Trends and Prediction Models for Fatigue Crack Growth under Variable Amplitude Loading, ECN-R-96-007, Netherlands Energy Research Foundation ECN, Petten, The Netherlands.
18. Stephens, R.I., Chen, D.K. and Hom, B.W. (1976). Fatigue Crack Growth under Spectrum Loads, ASTM STP 595, pp. 27-40.
19. Verma, B.B., Atkinson, J.D. and Kumar, M. (2001). Study of Fatigue Behavior of 7475 Aluminium Alloy, Bull. Mater. Science, 24(2): 231-236.
20. Wei, L.W., de Los Rios, E.R. and James, M.N. (2002). Experimental Study and Modeling of Short Fatigue Crack Growth in Aluminum Alloy A 7010-T7451 under Random Loading, International Journal of Fatigue, 24(9): 963-975.
21. Wu, Newman, Zhao, Swain, Ding and Phillips (1998). Small Crack Growth and Fatigue Life Predictions for High-Strength Aluminium Alloys - Part I: Experimental and Fracture Mechanics Analysis, J. Fatigue & Fracture of Engineering Materials and Structures, 21(11): 1289.