• 한국해양공학회지
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• 제7권2호
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• pp.131-140
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• 1993

To study the corrosion fatigue begavior of T.M.C.P. steel, the rotary bending fatigue test with the change of concentration of NaCl solution was carried out. Fatigue life in the corrosion environment is decreased markedly in comparision with that in the air. Fatigue limit in the air was about 225 MPa. In case of 3.5% NaCl solution fatigue life could be expressed as .sigma./sub f/=10,392 * (N/sub f/)/sup -o.2923 . According to the paris's rule, crack growth rates could be expressed as da/dN=2.62.*10/sup -7/ .DELTA. K/sup 1.09/(3.5% NaCl solution), da/dN=1.95 *10/sup -7 .DELTA. K/sup 1.05/(1% NaCl solution), da/dN=2.62 * 10/sup -7/.DELTA./sup 0.72/(0.01% NaCl solution) with da/dN expressed in mm/cycle and .DELTA.K in MPa.GAMMA.m. The crack growth rate in the corrosion environment was highest under 3.5% NaCl solution.

• 한국해양공학회지
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• 제9권1호
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• pp.92-100
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• 1995

The effect of different anisotropy and stress ratio on fatigue crack propagation behavior was investigated under various stress ratio(R=-0.4, -0.2, 0.2, 0.2, 0.4) using pure titanium sheet used in aerospace, chemical and food industry. The rack closure behavior under constant load amplitude fatigue crack propagation test was examined. Fatigue crack propagation rate da/dN was estimated in terms of effective stress intensity factor range, $\Delta$K$_{eff}$, regardless of various stress ratio but was influenced by anisotropy. Also, it was found that the effect of anisotropy was considerably decreased but still not negligible when he da/dN was evaluated by a conventional parameter, $\Delta$$K_{eff}$/E and when the modified da/dN.$\sqrt{\varepsilon}_f$ was evaluated by $\Delta$$K_{eff}$/E. On the other hand, da/dN could be evaluated uniquely by effective new parameter, $\Delta$K$_{eff}$/$sigma_{ys}$, regardless of anisotropy, as int he following equation da/dN=C''[\frac{{\Delta}K_{eff}}{{\sigma}_{ys}}]^{n''}. And effective stress intensity factor range ratio, U was estimated by the following equation with respect to the ratio of reversed plastic zone size, $\Delta r_{p}$ to monotonic plastic zone size, $r_p$ regardless of stress ratio and anisotropy. U=-4.45$(\Delta r_{p}/r_{p})^{2}$+4.1$(\Delta r_{p}/r_{p})$+0.245_{p})$+0.245

• 대한토목학회논문집
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• 제4권2호
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• pp.133-142
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• 1984

횡방향(橫方向)과 종방향(縱方向), 대입열용접(大入熱鎔接)과 소입열용접(小入熱鎔接), 모재(母材)와 같은 강도(强度)의 용접재료(鎔接材料) 사용(使用)과 모재(母材)보다 낮은 강도(强度)의 용접재료(鎔接材料) 사용(使用) 등으로 서로 비교되는 용접(鎔接)이음의 소인장시험편(小引張試驗片)을 만들어서 피로시험(疲勞試驗)을 행하여 피로구열(疲勞龜裂) 진전속도(進展速度) ${\frac{da}{dN}}$와 구열선단(龜裂先端) 부근의 응력확대계수(應力擴大係數)의 변동범위(變動範圍) ${\Delta}K$와의 관계곡선(關係曲線)을 그려서 비교시험간(比較試驗間)의 모재(母材), 열영향부(熱影響部) 및 용착금속부(鎔着金屬部)로 구분, 혹은 지금까지의 연구자료(硏究資料) 등과 비교검토하였다. 이 결과, 다음과 같은 현상들을 알 수 있었다. 기본적(基本的)으로, 용접방향(鎔接方向), 용접입열량(鎔接入熱量), 용접재료(鎔接材料)의 강도(强度), 혹은 모재(母材), 열영향부(熱影響部) 및 용착금속부(鎔着金屬部)의 구분 등에 따라 ${\frac{da}{dN}}-{\Delta}K$관계에 큰 차이가 없었다. 다만, 첫째, 소재(素材)에 대한 경우에 비해 대개 처음은 같은 ${\Delta}K$에서 ${\frac{da}{dN}}$가 상당히 늦다가 점차 증가하여 중간쯤에서 같아진 후 끝 부분에서 같은 ${\Delta}K$에서${\frac{da}{dN}}$가 다소 빨라짐을 알 수 있었다. 둘째, 열영향부(熱影響部)에서 용접금속부(鎔接金屬部)로 진전(進展)하면서 ${\frac{da}{dN}}$가 다소 늦어지는 것을 알 수 있었다. 셋째, 용접방향(鎔接方向)과 구열방향(龜裂方向)이 평행인 경우가 직각인 경우에 비해, 모재(母材)와 같은 용접재료(鎔接材料)를 쓴 경우 소입열용접(小入熱鎔接)인 경우가 대입열용접(大入熱鎔接)인 경우에 비해, 모재(母材)보다 낮은 용접재료(鎔接材料)를 쓴 경우 대입열용접(大入熱鎔接)인 경우가 소입열용접(小入熱鎔接)인 경우에 비해, 대입열(大入熱)의 평행용접(鎔接)의 경우를 제외한 모든 용접(鎔接)에서 모재(母材)와 같은 강도(强度)의 용접재료(鎔接材料)를 쓴 경우가 모재(母材)보다 낮은 강도(强度)의 용접재료(鎔接材料)를 쓴 경우에 비해 ${\Delta}K$가 낮은 시기(時期)에 일찍 저속(低速)으로 구열(龜裂)이 시작되어 ${\Delta}K$의 큰 증가없이 ${\frac{da}{dN}}$가 빠르게 증가한 다음 다른 경우와 같은 성상(性狀)으로 진전됨을 알 수 있었다. 넷째, 소입열용접(小入熱鎔接)의 경우 평행용접(鎔接)이 직각용접(鎔接)에 비해, 소입열용접(小入熱鎔接)이 대입열용접(大入熱鎔接)에 비해 같은 ${\Delta}K$에서 ${\frac{da}{dN}}$가 다소 늦은 것을 알 수 있었다.

• Steel and Composite Structures
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• 제17권2호
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• pp.145-157
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• 2014

This study aimed to investigate the fatigue crack growth behavior of a kind of fiber metal laminates (FML) under four different stress levels. The FML specimen consists of three 2024-T3 aluminum alloy sheets and two layers of glass/epoxy composite lamina. Tensile-tensile cyclic fatigue tests were conducted on centrally notched specimen at four stress levels with various maximum values. A digital camera system was used to take photos of the propagating cracks on both sides of the specimens. Image processing software was adopted to accurately measure the length of the cracks on each photo. The test results show that: (1) a-N and da/dN-a curves of FML specimens can be divided into transient crack growth segment, steady state crack growth segment and accelerated crack growth segment; (2) compared to 2024-T3 aluminum alloy, the fatigue properties of FML are much better; (3) da/dN-${\Delta}K$ curves of FML specimens can be divided into fatigue crack growth rate decrease segment and fatigue crack growth rate increase segment; (3) the maximum stress level has a large influence on a-N, da/dN-a and da/dN-${\Delta}K$ curves of FML specimens; (4) the fatigue crack growth rate da/dN presents a nonlinear accelerated increasing trend to the maximum stress level; (5) the maximum stress level has an almost linear relationship with the stress intensity factor ${\Delta}K$.

• 한국기계가공학회지
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• 제14권2호
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• pp.112-120
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• 2015

In this study, the growth rate of surface cracks (da/dN) during the retardation period was analyzed in terms of effective stress intensity factor range(${\Delta}K_{eff}^*$) obtained by using the proposed effective plastic zone concept. Effective stress intensity factors obtained by using the effective plastic zone concept were smaller than those obtained by using Willenborg analysis. On the growth rate of surface cracks analyzed by ${\Delta}K$, the dependence of overload stress levels appears. On the growth rate by ${\Delta}K_{eff}$ obtained by Willenborg analysis, there is a linear relationship with two different slops between da/dN and ${\Delta}K_{eff}$. However, on the growth rate by ${\Delta}K_{eff}^*$ obtained by the proposed effective plastic zone concept, there is a linear relationship between da/dN and ${\Delta}K_{eff}^*$ that coincides with the results of constant amplitude loading.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2001년도 추계학술대회 논문집
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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.

• 한국기계가공학회지
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• 제11권5호
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• pp.13-20
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• 2012

In order to clarify the effect of overload on crack growth behaviors, fatigue tests for overload were carried out for round plain specimens of SM45C steel. In the experiment, typical semi-elliptical crack shape was found and further crack growth behaviors were tested. Using three types of single overload fatigue tests, Crack growth retardation phenomenon were examined. The growth rate of surface crack(da/dN) during retardation period was analyzed in terms of ${\Delta}K$ and ${\Delta}K_{eff}$. On the growth rate of surface crack analyzed by ${\Delta}K$, the dependence of overload stress levels appears. However, on the growth rate by ${\Delta}K_{eff}$ obtained by Willenborg analysis, there is a non-liner relationship between da/dN and ${\Delta}K_{eff}$ with narrow scatter band.

• 한국기계가공학회지
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• 제11권4호
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• pp.82-89
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• 2012

In order to clarify the effect of overload on crack growth behaviors, fatigue tests for overload were carried out for round plain specimens of SM45C steel. In the experiment, typical semi-elliptical crack shape was found and further crack growth behaviors were tested. Using three types of single overload fatigue tests, Crack growth retardation phenomenon were examined. The growth rate of surface crack(da/dN) during retardation period was analyzed in terms of ${\Delta}K$ and ${\Delta}K_{eff}$. On the growth rate of surface crack analyzed by ${\Delta}K$, the dependence of overload stress levels appears. However, on the growth rate by ${\Delta}K_{eff}$ obtained by Willenborg analysis, there is a liner relationship between da/dN and ${\Delta}K_{eff}$ with narrow scatter band.

• 대한기계학회논문집
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• 제10권1호
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• pp.62-69
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• 1986

본 연구에서는 표면균열의 전파거동에 관한 연구의 일환으로 경량화재료 로서 항공기 구조용으로 널리 사용되고 있는 7075-T651 알루미늄합금을 준비하고 제하탄성 compliance법을 이용하여 표면 및 깊이 방향의 균열진전거동의 특성을 밝히고져 한다.

• Journal of Advanced Marine Engineering and Technology
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• 제15권1호
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• pp.51-58
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• 1991

Corrosion fatigue test was performed by the use of plane bending fatigue tester in marine environment having various specific resistance from 25(natural sea water) to 5000.ohm.cm. It is in order to investigate the effects of marine environmental factor on the corrosion fatigue fracture of SS41 steel. The main results obtained are as follows; 1. The aspect ratio(b/a) of corner crack growing in natural sea water is lower than that in air. 2. The surface crack growth rate(da/dN) in marine environment is faster than that in air and da/dN delaies with the specific resistance increased. 3. The experimental constant m of paris rule [da/dN=C(${\delta}$K)$^m$] decrease with the specific resistance decreased and the effect of corrosion in proportion to the specific resistance is more sensitive than that of stress intensity factor range(${\delta}$K) under region II. 4. The accelerative factor(${\alpha}$) in marine environment is about 1.1-2.7 and .alpha. is increase under the low region of stress intensity factor range(${\delta}$K). 5. The electrode potential($E_0$) gets less noble potential with the specific resistance decreased.