• Title/Summary/Keyword: 피로크랙개구거동

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Analysis of Fatigue Crack Opening: Belhlavioll Using Direct Measuring Method (직접측정법에 의한 피로크랙 개구거동의 해석)

  • Song, Sam-Hong;Kim, Hyun
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.16 no.8
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    • pp.1493-1502
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    • 1992
  • The purpose of this study is to identify the effects of loading variables on fatigue crack opening behavior, using structural steel SS41. To use various stress ratios, three kinds of the methods varying stress ratio were used; .DELTA.P const., P$_{max}$ const., and P$_{min}$ const.. To measure the opening load, the direct measuring method which measures the distance between two micro indentations 20 .mu.m behind crack tip and the elastic compliance method were used. As the results of present study, the following conclusions are obtained. First, using the direct measuring method, it was possible to measure the COD at any location behind crack tip. Second, as measuring point becomes farther from crack tip, opening load becomes smaller. Third, the acceleration of da/dN near notch is due to crack opening behavior. Finally, opening ratio is a function of not only R, but .DELTA.K.K.K.

Fatigue Short Cracks-Critical Aspect of Non-Propagation and Tolerant Microflaw (피로 미소크랙의 정류현상과 허용결함 크기와의 관계)

  • Kim, Min Gun
    • Journal of Industrial Technology
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    • v.8
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    • pp.39-46
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    • 1988
  • 탄소강 평활재 및 미소결함재를 사용하여, 미소 정류크랙의 크랙 개폐구거동의 상세한 관찰과 초기결함을 상정한 미소 원공과의 상호 한계크기의 비교 검토를 통하여, 다음과 같은 결론을 얻었다. 평활재의 정규크랙은, 피로과정중에 압축잔류응역이 크랙선단의 개구를 억제하는 것에 의하여 정류하게 되고, 그 크기는 평활재의 피로한도를 저하시키지 않은 미소 원공의 한계크기와 거의 일치하여, 두 경우가 역학적으로 거의 등가함을 시사해 주고 있다.

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The Finite Element Analysis of Fatigue Crack Opening Behavior Using Two Dimensional Eight Node Isoparametric Element (2차원 8절점 등매개요소를 사용한 피로크랙개구거동의 유한요소해석)

  • Song, Sam-Hong;Kim, Hyun
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.18 no.2
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    • pp.271-277
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    • 1994
  • The fatigue crack opening behavior is analyzed using finite element method. Because extremely fine mesh subdivision is required when using constant stress constant strain triangular element, this study uses conventional two dimensional eight node isoparametric elements. Since plasitc zone size is similar to crack propagating length per each load cycle because of relatively large element size, a new analysis model that a crack propagates every two load cycle is suggested. the opening load and crack opening displacement can be obtained accurately by this method.

LASER ISDG법으로 관찰한 용접재에서의 피로크랙개구거동

  • 송삼흥;김현;최진호
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2001.10a
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    • pp.263-268
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    • 2001
  • The constant .DELTA. K fatigue tests are performed in SS41 and its weldment. The LASER ISDG method is used in determination of crack opening ratio. This method is more precise than indirect measurement method, faster and easier than other direct measurement method. And obtained results are followed 1) Crack opening ratio U is proportional to fatigue crack growth rate da/dN at constant .DELTA. K 2) Fatigue crack growth rate da/dN in weldment increases in weld metal and heat affected zone, decreases in base metal as crack grows.

A Study on the Fatigue Crack Propagation Behavior in the SB41 Welding Material (SB41용접재의 피로크랙 진전거동에 관한 연구)

  • 최병기;장경천
    • Transactions of the Korean Society of Machine Tool Engineers
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    • v.11 no.2
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    • pp.43-49
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    • 2002
  • SB41 material is welded automatically and is investigated some effects of the welding residual stress in the growth and propagation of fatigue crack, so as to study the fatigue behaviour in the welding residual stress field. The summarized results are as follows; 1) In case of the load amplitude is constant, as the stress ratio is changing to 0.1, 0.33 and 0.5 the propagation life is constant but the growth life decreases. And than, when maximum load or minimum load is constant as the stress ratio increases the growth life and propagation life. 2) It was shown that fatigue crack propagation ratio da/dN was almost constant regardless of the stress ratio change at constant load amplitude and that the larger stress ratio, the slower was the fatigue crack propagation ratio. 3) The opening ratio U is influenced by $K_max$ but it isn't only the function of $K_max$ because data range is very large. 4) The fatigue life of the specimens on tensile compressive residual stress field was decreased and increased respectably more than that of the base metal.