• 한국정밀공학회지
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• 제9권1호
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• pp.106-117
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• 1992

In this study, the propagation behaviour and the closure phenomena of physically small surface cracks were investigated by the techinque of the Kikukawa-unloading elastic compliance method using a back face strain gage. The surface cracks initiated and propagated from notched specimens under constant amplitude bending load. The crack shape (aspect ratio) with approximately semi-circular at the early stage was changed to semi-elliptical as the cracks grew larger. The crack depth (a) could be expressed uniquenly by the crack length (c). The dependence of the crack propagation rate on the stress ratio R was strongly related in the lower ${\Delta}K$ range. The deceleration of the surface crack propagation rate was prominent in lower R during the crack length was small. When the propagation rate was rearranged with the effective stress intensity factor range ${\Delta}$K_{eff} the dependence of the crack propagation rate on the stress ratio R was found to be diminshed. These were caused by the crack closure phenomena that was most prominent at the lower propagation rate. The mechanism of crack closure phenomena was dominated by the plasticity-induced mechanism.

• 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

• 콘크리트학회논문집
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• 제20권4호
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• pp.523-530
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• 2008

구조설계기준에서, 슬래브의 최대 펀칭전단응력은 연직하중에 의한 직접전단과 불균형모멘트에 의한 편심전단의 조합응력으로 규정하고 있다. 이것은 슬래브에 작용하는 펀칭전단응력에 불균형모멘트의 영향을 반영한 것이다. 그러나 부재의 저항성능 즉 펀칭전단강도에는 슬래브의 불균형모멘트강도 영향을 전혀 고려하고 있지 않다. 본 논문에서는 불균형모멘트-펀칭전단 상관모델을 제시하였다. 상관모델에서 불균형모멘트와 펀칭전단의 하중영향 및 저항성능 관계는 2차원으로 표현된다. 상관모델을 이용하여, "슬래브의 펀칭전단강도를 결정하는데 있어 불균형모멘트강도를 어떻게 반영할 것인지"에 대한 방안을 제시하였다. 또한, 전단보강재가 불균형모멘트강도에 미치는 영향을 분석하고 이를 구조설계에 반영하기 위한 유효폭확대계수의 적용을 제안하였다. 본 논문에서 제시한 상관모델은 하중과 전단보강재에 따른 펀칭전단과 불균형모멘트 강도를 실제 거동에 가깝게 정의할 수 있고 슬래브의 휨지배파괴 또는 전단지배파괴의 최종적인 파괴모드를 쉽게 예측할 수 있어 슬래브의 구조적 거동을 예측하는데 매우 효과적이다.