• 대한기계학회논문집A
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• 제37권3호
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• pp.345-352
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• 2013

본 논문에서는 광탄성 실험 하이브리드 법을 이용하여 접촉응력문제를 해석하는 경우의 응력형상 함수에 대해서 다루고 있다. 일반적으로 접촉응력문제는 반평면 문제로써 해석 되어지므로, 접촉응력의 경우 Airy 응력함수를 구성하는 두 해석적인 응력함수의 관계는 균열문제에서와 유사하였다. 그러나 이 관계를 그대로 접촉응력문제 (특히 특이점을 가진 경우)에 사용할 수가 없다. 그러므로 정확한 접촉문제의 해석을 위해 이들 두 해석적인 응력함수의 형태에 접촉하는 두 끝점의 조건에 따른 응력형상함수를 반드시 고려하여야만 할 것이다. 두 접촉끝점의 응력 특이성에 따라 4종류로 분류되는 이들 응력형상함수 중에서 오링 해석을 위한 중요한 두 종류의 응력형상함수를 선택하였으며, 이것의 유효성을 검증하였다.

• 한국자동차공학회논문집
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• 제4권1호
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• pp.55-62
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• 1996

The dynamic photoelastic technique has been utilized to investigate the possibility of relieving the large local singular stresses which are induce in the corner of a right angled indenter. The indenter compresses a semi-infinite body dynamically with an impact load applied on the top of the indenter. The effect of geometric changes to the indenter in terms of the diameter (d) and the location (ℓ) of the notch on the relieving of the dynamic contact stresses are investigated. A multi-spark-high speed camera with twelve sparks was used to take dynamic photographs. The contact singular stresses were found to be released by introducing the relief notch along the indenter. The optimal location and geometry of the relief notch need further experimental investigation.

• 대한기계학회논문집A
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• 제20권7호
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• pp.2097-2107
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• 1996

The dynamic photoelastic technique had been utilized to investigate the possibillity of relieving the large local singular stresses induced at the corner of a right- angle- indenter. The indenter compressed a semi-infinite body dynamically with an impact load applied on the top of the indenter. The effects of the geometric changes of the indenter in terms of the diameter (d) and the location (1) of the stress relieving notch on the behavior of the dynamic contact stresses were investigated. The influence of stress relieving notches positioned along the edge of the semi-infinite body on the dynamic contact stresses were also studied by changing the diameter (D) and the location (L) of the notch. A multi-speak-high speed camera with twelve sparks were used to take photographs of full field dynamic isochromatic fringe patterns. The contact singular stresses were found to be released significantly by the stress relief notches both along the indenter and the edge of the semi-infinite body. The optimal position and geometry of the stress relieving notches were obtained with the aid of limited experimental results.

• 대한기계학회논문집A
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• 제39권6호
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• pp.583-588
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• 2015

완전접촉 문제를 이론적으로 해석하기 위해서 점근해법이 많이 사용된다. 점근해로서의 응력장은 특이항 만으로 구성되므로 접촉경계로부터 멀어질수록 정확도가 감소한다. 이에 반해 유한요소해석 방법은 요소크기의 제한으로 인해 완전접촉 문제에서의 응력특이성을 엄밀히 표현할 수 없다. 따라서 본 연구에서는 이론적 해법을 보조하고 또 그와 비교하기 위해 응착접촉 상태에 있는 완전접촉 문제를 이론적으로 해석한 후, 모아레 실험 및 유한요소해석 방법으로 접촉부 부근의 응력장을 분석하였다. 실험은 알루미늄과 구리 합금을 접촉각 $120^{\circ}$, $135^{\circ}C$로 가공하여 수행하였으며 모아레 무늬로부터 얻은 변위장과 유한요소해석을 수행한 결과와 비교하였다. 이로부터 타당성이 확보된 수치적 방법을 이용하여 실험조건에서의 일반화 응력확대계수와 접촉부 응력장을 구하여 이론 해와 비교하였으며, 접촉경계로부터 멀어질 때 나타나는 이론과 수치 해의 차이를 분석하였다.

• 대한기계학회논문집A
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• 제20권1호
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• pp.180-188
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• 1996

The stress singularity of a sharp wedge contacting a half plane can be avoided by changing the wedge shape. Shape optimization is accomplished with the geometric strain method (GSM), an optimality criterion method. Several numerical examples are provided for different materials in the wedge and half plane to avoid stress singularity neal the sharp corner of the wedge. Optimum wedge shapes are obtained and critical corner angles are compared with the angles from analytical contact mechanics. Numerical results are well matched to analytical and experimental results. It is shown that shape optimization by the geometric strain method is a useful tool to reshape the wedge and to avoid a stress singulatiry. The method applies to more general geometries where the singular behavior would be difficult to avoid by classical means.

• 한국정밀공학회지
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• 제16권4호통권97호
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• pp.197-204
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• 1999

The boundary element method was used for studying singularities of an interface crack with contact zones. The iterative procedure is applied to estimate the contact zone size. Because the contact zone size was extremely small in a tension field, a large number of Gaussian points were used for numerical integration of the Kernels. Stress extrapolation method and J-integral were used ofr determining stress intensity factors. When the interface crack was assumed to have opened tips, oscillatory singularities appear near the tips of the interface crack. But the interface crack with contact zone which Comninou suggested had no oscillatory behavior. The contact zone size under shear loading was much larger than that under tensile. The stress intensity factors computed by stress extrapolation method were close to those of Comninou's solution. And the stress intensity factor evaluated by J-integral was similar to that by stress extrapolation method.

• Tribology and Lubricants
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• 제35권4호
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• pp.229-236
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• 2019

This study investigates the stress singularity that occurs at the contact edge of three bodies in a frictional complete contact. We use the asymptotic analysis method, wherein we constitute an eigenvalue problem and observe the eigenvalue behavior, which we use to obtain the order of the stress singularity. For the present geometry of three bodies in contact, a contact between a cracked indenter and half plane is considered. This is a typical geometry of the PCMI problem of a nuclear fuel rod. Thus, this paper, specifically presents the characteristics of the PCMI problem from the perspective of stress singularity. Consequently, it is noted that the behavior of the stress singularity varies with the difference in the crack angle, coefficient of friction, and material dissimilarity, as is observed in a frictional complete contact of two bodies. In addition, we find that the stress singularity changes essentially linearly with respect to the coefficient of friction, regardless of the variation in the crack angle and material dissimilarity. Concurrently, we find the order of singularity to be 0.5 at a certain coefficient of friction, irrespective of the crack angle, which we also observe in the crack problem of a homogeneous and isotropic body. The order of singularity can also exceed 0.5 in the frictional complete contact problem of three bodies. This implies that the propensity for failure when three bodies are in frictional complete contact can be even worse than that in case of a failure induced by a crack.