• 대한기계학회논문집
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• 제15권3호
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• pp.931-935
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• 1991

본 연구에서는 유효응력확대계수로서 피로크랙 진전수명을 평가할 수 이용되 는 크랙열림비(본 논문에서는 후술하는 최대응력에 대한 크랙 열림응력의 비를 크랙 열림비로 하다)가 진전수명에 미치는 영향을 평가하기 위한것으로서, 제1보에서는 실 험에 의하여 크랙 열림점을 실측한 결과 측정입치에 따라 다른 값을 나타내며 수명평 가법 크랙 선단으로부터 떨어진 곳(크립게이지를 이용한 크랙마우스등)에서 측정한 크 랙 열림점 값을 이용함이 보다 정확함을 밝혔다.본 제2보에서는 크랙열림비가 수명 평가에 미치는 영향을 상기의 파라미터 영향도 평가수법을 이용하여 평가하고자 한다.

• 대한기계학회논문집A
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• 제20권7호
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• pp.2234-2245
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• 1996

In this study residual stress in weldment was considered about the effect on the fatigue propagation and about the effect of redistribution of residual stress. Then, fatigue tests were conducted by the center notched specimens machined with welded plate. The residual stress and its redistribution after the crack growth were measured by the magnetizing stress indicator and hole-drilling method. Fatigue crack propagation was estimated by the specimens having residual stress redistributed after the cracks growth and having the effects of crack closure. Crack growth rates were predicted and compared with experimental results. It had been found that the predicted crack propagation rates have a good agreement with experimental results when the redistribution of residual stress was considerd.

• 대한조선학회논문집
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• 제41권6호
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• pp.84-90
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• 2004

For the precise assessment of the effect of welding residual stresses on structural strength and fatigue crack growth behavior, new FE analysis algorithms for the estimation of residual stress relaxation due to external load and redistribution due to fatigue crack propagation were proposed in this paper. Initial welding residual stress field was obtained by thermal elasto-plastic analysis considering temperature dependent material properties, and the amount of residual stress relaxation and redistribution were assessed by subsequent elasto-plastic analysis In the analysis of fatigue crack propagation, the applied SIF(Stress Intensity Factor) range was evaluated by $\frac{1}{4}$-point displacement extrapolation method, and the effect of welding residual stresses on crack propagation was considered by introducing the effective SIF concept. The test results of crack propagations were compared with the predicted data obtained by the analysis.

• 한국생산제조학회지
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• 제9권5호
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• pp.73-79
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• 2000

The applications of fracture mechanics have traditionally concentrated on cracks loaded by tensile stresses, and growing under an opening or mode I mechanism. However, many cases of failures occur from growth of cracks subjected to mixed mode loading. Several criteria have been proposed regarding the crack growth direction under mixed mode loadings. This paper is aimed at investigation of fatigue crack growth behaviour under mixed mode(I＋II) with variation of angle and pre-crack length in two dimensional branched type precrack. Especially the direction of fatigue crack propagation was predicted and effective stress intensity factor was calculated by finite element analysis(FEA. In this paper, the maximum tangential stress(MTS) criterion was used to predict crack growth direction. Not only experiment but also finite element analysis was carried out and the theoretical predictions were compared with experimental results.

• 한국해양공학회지
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• 제4권1호
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• pp.81-87
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• 1990

Fatigue crack closure levels based on the behavior of residual displacements on crack surfaces, are determined analytically according to the microscopic crack closure mechanisms, i.e., whether the first contact of crack surfaces takes place at the very crack tip or on the surfaces near the tip. The comparative analysis on the two models is carried out empirically by the constant amplitude fatigue tests on 2024-T3 aluminum alloy plate, and it shows that under negative stress ratio, the case of the first contact at crack tip gives better agreement with the experimental results than the other.

• 한국해양공학회지
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• 제4권1호
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• pp.87-87
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• 1990

Fatigue crack closure levels based on the behavior of residual displacements on crack surfaces, are determined analytically according to the microscopic crack closure mechanisms, i.e., whether the first contact of crack surfaces takes place at the very crack tip or on the surfaces near the tip. The comparative analysis on the two models is carried out empirically by the constant amplitude fatigue tests on 2024-T3 aluminum alloy plate, and it shows that under negative stress ratio, the case of the first contact at crack tip gives better agreement with the experimental results than the other.

• 한국기계가공학회지
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• 제5권2호
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• pp.42-48
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• 2006

In order to assess the validity of fatigue crack arrest design charts obtained from our previous numerical approach to fatigue crack arrest condition, an extensive fatigue crack growth/arrest test was performed using CT-type integrally stiffened panels. The results are presented as fatigue crack growth rate and non-dimensional crack length relationship, and these are compared with numerically simulated crack growth rates. The measured values of da/dN at the moment of fatigue crack arrest occurred in stiffened panels are good agreement with those numerically simulated crack growth rates.

• 대한조선학회논문집
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• 제29권2호
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• pp.79-91
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• 1992

본 논문에서는 균열 보수에 사용되는 Patch와 균열진 판 사이에 컴프라이언스 개념을 적용하여 Patch된 균열진 판의 응력확대계수를 이론유도하고, 이에 대한 실험과 균열진전 거동규명을 통하여 그 유효성을 충분히 검증하였다. 또한, 이와같은 컴프라이언스를 이용한 이론방법을 바탕으로 균열진 구조물의 잔존수명이 고려된 Patch를 간단히 설계할 수 있는 기법을 제시하였다.

• 대한기계학회논문집A
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• 제35권11호
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• pp.1415-1422
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• 2011

운송기계구조물의 제작에 사용되는 판재 알루미늄 합금재료는 일정한 피로응력조건하에서 두께에 따라 균열진전속도의 차이를 보인다. 이러한 두께효과는 판재 알루미늄합금의 주요한 피로파괴특성 중 하나이다. 본 연구에서는 일정한 피로응력조건하에서 실시한 후판 및 박판 Al 2024-T3 합금재료의 피로 시험을 통하여 두께효과를 파악하고, 이를 형상인자인 두께비, $R_t$ 및 하중인자인 두께별 등가유효응력확대비, $U_{i}^{equ}$에 의한 상호관계식, $U_{i}^{equ}=f(R_t)$로 나타내었다. 그리고 두께효과에 의한 후판 대비 박판시험편의 균열진전 지연거동을 ${\Delta}K$ 환산법을 사용하여 정량적으로 분석하였다. 두께효과의 경향을 정량으로 나타내기 위해 두께감소율(DoT)과 응력확대계수범위, ${\Delta}K$의 감소율(DoS) 등의 값을 구하여 이들 상호관계를 규명하였다.

• 대한기계학회논문집A
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• 제35권11호
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• pp.1361-1368
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• 2011

응력확대계수비와 하중 주파수가 각각 'R=0.1, f=0.1 Hz', 'R=0.3, f=0.3 Hz' 및 'R=0.5, f=0.5 Hz'인 세가지 하중 조건에서 피로균열전파 실험을 하였으며 이를 바탕으로 고성능 강재의 피로균열전파거동 분석과 피로수명평가를 수행하였다. 하중 조건에 따른 피로균열전파거동을 모사하기 위해 수정된 Forman 모델을 제안하였으며 제안된 모델은 하한 응력확대계수폭과 균열 닫힘 현상에 의한 유효 응력확대계수폭을 고려함으로써 거동의 전 영역을 모사할 수 있었다. 응력확대계수비와 하중 주파수가 0.1 인 경우, 균열이 약 5.0 mm 전파될 때 피로수명을 평가한 결과, Forman 모델은 8,814 cycles, 수정된 모델은 12,292 cycles 의 계산결과를 얻었으며, 이를 12,774 cycles 의 실제 실험결과와 비교할 때 수정된 Forman 모델이 실제 피로균열전파거동을 보다 효과적으로 모사하고 있음을 확인할 수 있었다.