Estimations of fatigue life and variability under random loading in aluminum Al-2024T351 using strip yield models from NASGRO

Abstract This paper is concerned with the application of the strip yield models implemented in NASGRO to estimate fatigue crack growth under random loading. The two different strip yield model options (constant constraint-loss (CCL) and variable constraint-loss (VCL)) implemented in the software are considered and compared. In addition, three crack grow rate relations, obtained from constant amplitude data, the NASGRO material database and the literature, were also considered and compared. The capacity of the models to estimate the fatigue life and variability is analyzed by comparing simulated results with experimental data of fatigue crack growth under different stationary Gaussian random load processes on compact, C(T), specimens of aluminum alloy 2024-T351. The analysis performed showed that both model options provide very similar good fatigue life predictions. The estimated fatigue lives are within ±13% of the test lives with the best option. The variability of the results due to the randomness of the load is also analyzed. In this case, the variable constraint-loss option provides better estimation than the constant constraint-loss option.

[1]  J. Domínguez,et al.  On the use of the strip-yield model to predict fatigue crack growth under irregular loading , 1997 .

[2]  J. Newman A crack opening stress equation for fatigue crack growth , 1984 .

[3]  J. C. Newman,et al.  Crack-growth calculations in 7075-T7351 aluminum alloy under various load spectra using an improved crack-closure model , 2004 .

[4]  J. Schijve,et al.  Application of the strip-yield model from the NASGRO software to predict fatigue crack growth in aluminium alloys under constant and variable amplitude loading , 2007 .

[5]  David J. Smith,et al.  Predictions of fatigue crack growth in aluminium alloy 2024–T351 using constraint factors , 2001 .

[6]  D. S. Dugdale Yielding of steel sheets containing slits , 1960 .

[7]  Christopher D. Glancey,et al.  Fatigue crack growth and life predictions under variable amplitude loading for a cast and wrought aluminum alloy , 2006 .

[8]  W. Elber The Significance of Fatigue Crack Closure , 1971 .

[9]  Jaime Domínguez,et al.  Effect of load histories on scatter of fatigue crack growth in aluminum alloy 2024-T351 , 1997 .

[10]  Tomasz Machniewicz Fatigue crack growth prediction models for metallic materials Part II: Strip yield model - choices and decisions , 2013 .

[11]  Jaime Domínguez,et al.  Numerical and experimental analysis of fatigue crack growth under random loading , 2005 .

[12]  Jaime Domínguez,et al.  An experimental analysis of fatigue crack growth under random loading , 2003 .

[13]  Effects of crack closure on fatigue crack-growth predictions for 2024-T351 aluminum alloy panels under spectrum loading , 2007 .