Browse > Article

Effects by Applying Mode of Single Overload on Propagation Behavior of Fatigue Crack  

송삼홍 (고려대학교 공과대학 기계공학과)
이정무 (고려대학교 공학기술연구소)
Publication Information
Abstract
In this study, when variable-amplitude load with various applying mode acts on the pre-crack tip, we examined how fatigue cracks behave. Hence aspects of the deformation caused by changing the applying mode of single overload and propagation behavior of fatigue crack were experimentally examined: What kinds of the deformation would be formed at pre-crack and its tip\ulcorner What aspects of the residual plastic deformation field would be formed in front of a crack\ulcorner How aspects of the plastic zone could be evaluated\ulcorner As applying mode of single overloading changes, the deformation caused by tensile and shear loading variously showed in each applying mode. The different aspects of deformation make influence on propagation behavior of cracks under constant-amplitude fatigue loading after overloading with various modes. We tried to examine the relationship between aspects of deformation and fatigue behavior by comparing the observed deformation at crack and crack propagation behavior obtained from fatigue tests.
Keywords
Single overload; Mixed mode; Applying mode; Shear components; Residual plastic deformation field; Retardation;
Citations & Related Records
연도 인용수 순위
  • Reference
1 Richard, H. A. and Benitz, K., 'A Loading Device for the Criterion of Mixed Mode in Fracture Mechanics,' International Journal of Fracture, Vol. 22, pp. R55-R58, 1983   DOI
2 Richard, H. A., 'Some Theoretical and Experimental Aspects of Mixed Mode Fracture,' Advances Fracture Research, Vol. 5, pp. 3337-3344, 1986
3 Pook, L. P., 'The Effect of Crack Angle on Fracture Toughness,' Engineering Fracture Mechanics, Vol. 3, pp. 205-218, 1971   DOI   ScienceOn
4 Jones, R.E., 'Fatigue Crack Growth Retardation After Single-Cycle Peak Overload in Ti-6Al-4V Titanium Alloy,' Engineering Fracture Mechanics, Vol. 5, pp. 585-604, 1973   DOI   ScienceOn
5 Skorupa, M., 'Load Interaction Effects During Fatigue Crack Growth Under Variable Amplitude Loading-A Literature Review. Part II: Qualitative Interpretation,' Fatigue Fracture engineering Materials Structures, Vol. 22, pp. 905-926, 1998   DOI
6 Qian, J. and Fatemi, A., 'Mixed Mode Fatigue Crack Growth: A Literature Survey,' Engineering Fracture Mechanics, Vol. 55, No. 6, pp. 969-990, 1996   DOI   ScienceOn
7 Gao, Hua and Fernando, Upul. S., 'Effect of Non-Proportional Overloading on Fatigue Life,' Fracture Engineering Materials Structures, Vol. 19, No. 10, pp, 1197-1206, 1996   DOI   ScienceOn
8 Song, S. H. and Kwon, Y. K., 'A Study on Fatigue Crack Retardation and Retardation Mechanism in Variable Loading,' Transaction of the KSPE, Vol. 14, pp.76-81, 1997   과학기술학회마을
9 Elber, W., 'The Significance of Fatigue Crack Closure in Damage Tolerance in Aircraft Structure,' ASTM STP.924, pp. 230-242, 1971