On Three-Dimensional Fatigue Crack Propagation under Constant Amplitude Loading

Yu Ting He; Wen Jun Shu; Ren Yu Liu; Rong Hong Cui

doi:10.4028/www.scientific.net/AMR.97-101.852

Paper Titles

Characterization of Tensile Damage for 3D-C/SiC Composites by Acoustic Emission
p.834

Tempering Resistance of a New Type of Tool Steels Used in Magnesium Die Casting Machine
p.838

Influence of HLB Parameters of Surfactants on Properties of Magneto-Rheological Fluid
p.843

Experimental and Numerical Evaluation of the Vibration Fatigue of Small Bore Pipe in PWR
p.848

On Three-Dimensional Fatigue Crack Propagation under Constant Amplitude Loading
p.852

Strain-Based Fatigue Test and Reliability Research of 42CrMo Alloy Steel
p.856

Wear Behavior of Cr₂O₃/Cu Composite under Electrical Sliding
p.861

A New Electromechanical Coupling Model for Piezoelectric Actuator
p.867

Stress Relaxation Analysis of Polyurethane Foam Preloaded Structures
p.871

HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 97-101On Three-Dimensional Fatigue Crack Propagation...

On Three-Dimensional Fatigue Crack Propagation under Constant Amplitude Loading

Abstract:

The equation of fatigue crack propagation rate is indispensable to precisely predict the fatigue life of structure containing three-dimensional crack under constant amplitude loading. Considering the crack closure effects and thickness effects in real structures, the equation of fatigue crack propagation rate under tri-axial stress state is presented. And the fatigue propagation lives of LY12-BCZYU aluminium alloy plate specimens with central through crack are predicted by this equation and validated by experimental results. Validation against calculations by the model and experimental data shows a good agreement.

You might also be interested in these eBooks

View Preview

Info:

Periodical:

Advanced Materials Research (Volumes 97-101)

Pages:

852-855

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.97-101.852

Citation:

Cite this paper

Online since:

March 2010

Authors:

Yu Ting He, Wen Jun Shu, Ren Yu Liu, Rong Hong Cui

Keywords:

Constant Amplitude Loading, Crack Propagation Rate, Fatigue Life, Tri-Axial Stress State

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] Wanlin Guo: Eng. Fract. Mech. Vol. 49(1994), p.277.

Google Scholar

[2] Wanlin Guo: PhD thesis, Northwestern Polytechnical University (1991).

Google Scholar

[3] Y. T. He, F Li. and G.Q. Zhang. et al. ：AEPA2004, Shanghai, P.R. China(Sept. 22-26, 2004).

Google Scholar

[4] Elber W., in: Damage Tolerance In Aircraft Structures, ASTM STP 486, (1971), pp.320-242.

Google Scholar

[5] Y. T. He: PhD thesis, Northwestern Polytechnical University (1997).

Google Scholar

[6] Qingzhi He: Journal of Beijing Astronautics College Vol. 3(1981), p. l.

Google Scholar

[7] Tianyou Fan: Elementary fracture mechanics(Jiangsu Science and Technology Press, 1978).

Google Scholar

[8] Yuting He, in: Progress in Experimental an Computational Mech. In engineering and Material Behavior. Urumqi, China (1999).

Google Scholar

[9] Y. T. He, F. Li, R Shi, et al: Key Engineering Materials Vols. 297-300(2005).

Google Scholar

[10] Wu X R. Handbook of mechanical properties of aircraft structural metals. Vol. 2, Damage tolerance (Aeronautical Industry Press, China, Beijing, 1996).

Google Scholar

[11] Wu X R. Handbook of mechanical properties of aircraft structural metals. Vol. 1, Static Strength Fatigue /Durance, (Aeronautical Industry Press, China, Beijing, 1996).

Google Scholar

[12] X. L. Zheng: Quantitative theory on metal fatigue (Northwestern Polytechnical University press, China, Xi'an, 1994).

Google Scholar

[13] Budiansky B., Hutchinson J. W.: J. Appl. Mech., Vol. 45(1978), pp.267-276.

Google Scholar

[14] Air structure strength institute, A test repot about crack propagation for Y7-200A aircraft carbine windshield frame material (LY12-BCZYU) under constant amplitude loading and typical stress spectrum (the number of report: Y7-9702), 1997, 9.

Google Scholar