Title of article
A theoretical model of semi-elliptic surface crack growth
Author/Authors
Shi، نويسنده , , Kaikai and Cai، نويسنده , , Lixun and Chen، نويسنده , , Si long and Bao، نويسنده , , Chen، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2014
Pages
5
From page
730
To page
734
Abstract
A theoretical model of semi-elliptic surface crack growth based on the low cycle strain damage accumulation near the crack tip along the cracking direction and the Newman–Raju formula is developed. The crack is regarded as a sharp notch with a small curvature radius and the process zone is assumed to be the size of cyclic plastic zone. The modified Hutchinson, Rice and Rosengren (HRR) formulations are used in the presented study. Assuming that the shape of surface crack front is controlled by two critical points: the deepest point and the surface point. The theoretical model is applied to semi-elliptic surface cracked Al 7075-T6 alloy plate under cyclic loading, and five different initial crack shapes are discussed in present study. Good agreement between experimental and theoretical results is obtained.
Keywords
Linear damage accumulation , Low cycle fatigue , Newman–Raju formula , fatigue crack propagation , Semi-elliptic surface crack
Journal title
Chinese Journal of Aeronautics
Serial Year
2014
Journal title
Chinese Journal of Aeronautics
Record number
2265530
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