• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 1992년도 춘계학술대회 논문집
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• pp.268-273
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• 1992

Thin walled tubular specimens of 0.45% structural carbon steel were used in the bizxial tests. Biaxial fatigue tosts were conducted on strain control including fully reversed tension-compression and in phase tension torsion loadings. The predictions of the biaxial fatigue life were based upon the uniaxial low cycle fatigue test results. Fatigue lives were ranged from 10$\^$2/to 10$\^$5/cycles. Four multiaxial strain based theories have been developed to correlate biaxial fatigue experimdntal results. These theories showed good correlatins except for maximum shear strain theory. In uniaxial tests, crack behavior was observed that crack initiated in the maximum shear strain direction and propagated in the direction perpendicular to principal stross. But, in biaxial tests, both crack initiation and growth occured on the maximum shear strain direction only.

• 대한기계학회논문집A
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• 제25권5호
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• pp.874-882
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• 2001

The static and fatigue tests have been carried out to verify the validity of a generalized residual strength degradation model. And a new method of parameter determination in the model is verified experimentally to account for the effect of tension-compression fatigue loading of spheroidal graphite cast iron. It is shown that the correlation between the experimental results and the theoretical prediction on the statistical distribution of fatigue life by using the proposed method is very reasonable. Furthermore, it is found that the correlation between the theoretical prediction and the experimental results of fatigue life in case of tension-tension fatigue data in composite material appears to be reasonable. Therefore, the proposed method is more adjustable in the determination of the parameter than maximum likelihood method and minimization technique.

• 한국해양공학회지
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• 제18권6호
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• pp.84-90
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• 2004

Fatigue tests were conducted on SM45C steel using hour-glass shaped smooth tubular specimen under biaxial loading in order to investigate the crack formation and growth at room temperature. Three types of loading systems, were employed fully-reserved cyclic torsion without a superimposed static tension or compression fully-reserved cyclic torsion with a superimposed static tension and fully-reserved cyclic torsion with a superimposed static compression. The test results showed that a superimposed static tensile mean stress reduced fatigue life however a superimposed static compressive mean stress increased fatigue life. Experimental results indicated that cracks were initiated on planes of maximum shear strain whether or not the mean stresses were superimposed. A biaxial mean stress had an effect on the direction that the cracks nucleated and propagated at stage 1 (mode II).

• 대한기계학회논문집A
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• 제20권6호
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• pp.1836-1842
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• 1996

In this paper, static and fatigue bending strengths of CFRP(carbon fiber reinforced plastic laminates having impact damage(FOD) are evaluated. Composite laminates used for this experiment are CF/EPOXY and CF/PEEK orthotropy laminated plates, which have two-interfaces[${0^0}_4{90^0}_4}$]$_sym$. A steel ball launched by the air gun colides against CFRP laminates to generate impact damages. The damage growth during bending fatigue test is observed by the scanning acoustic microscope(SAM). When the impacted side is compressed, the residual fatigue bending strength of CF/PEEK specimen P is greater that that of CF/EPOXY SPECIMEN B. On the other hand, when the impacted side is in tension, the residual fatigue bending strength of CF/PEEK speicemen P is smaller than that of CF/EPOXY specimen B. In the case of impacted-side compression, fracture is proposed from the transverse crack generated near impact point. On the other hand, fracture is developed toward the impact point from the edge of interface-b delamination in the case of impacted-side tension.

• 대한기계학회논문집A
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• 제34권12호
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• pp.1821-1828
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• 2010

레이저 샥 피닝(LSP)은 금속재료 표면처리를 위한 획기적인 기술로서 금속 부품의 피로성능 개선을 위해 최근에 널리 적용되고 있다. 널리 알려진 바와 같이 금속재료의 피로 균열은 재료의 응력 상태가 인장(Tension)하에서만 발생되고, 압축(Compression)상태에서는 발생하지 않는다. 따라서 피로수명 개선을 위해 전통적인 샷 피닝(SP)과 함께 다양한 분야에 응용되고 있으며, 특히 LSP 는 금속재료의 표면과 깊이방향에 대해 높은 압축잔류응력을 생성시켜 준다. 본 논문에서는 유한요소 해석기법을 이용하여 LSP 에 의해 발생되는 압축잔류응력 생성과정을 모사하고, 압축잔류응력에 영향을 미치는 다양한 변수에 대해 민감도 해석을 수행하였다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 춘계학술대회논문집A
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• pp.298-303
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• 2000

A procedure to predict the fatigue life of rubber components based on the signed principal strain method was proposed. A tension-compression rubber specimen with Jang-gu shape was designed and principal strain distribution was obtained by using the nonlinear finite element analysis. Finite element analysis and fatigue test of strut rubber mount were conducted to evaluate the fatigue life prediction procedure proposed. A procedure was employed to predict the fatigue life of strut rubber mount. Predicted fatigue lives have a good agreement with tested lives within a factor of 3.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2004년도 춘계학술대회
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• pp.353-358
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• 2004

We got the following characteristics from fatigue crack growth test carried out in the environment of room temperature and low temperature at $25^{circ}C$, $-60^{circ}C$, $-80^{circ}C$, and $-100^{circ}C$ in the range of stress ratio of 0.3 by means of opening mode displacement. And there is a difference between shot peened specimen and unpeened specimen. The purpose of this study is to predict the behavior of fatigue crack propagation as one of fracture mechanics on the compressive residual stress. Fatigue crack growth rate of shot peened metal was lower than that of unpeened metal. The compressive residual stress made an impact on tension and compression of the plasticity deformation in fatigue crack plasticity zone. That is. the constrained force about plasticity deformation was strengthened by resultant stress, which resulted from plasticity deformation and compressive residual stress in the process of fatigue crack propagation.

• 대한기계학회논문집A
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• 제25권9호
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• pp.1452-1460
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• 2001

A new method of parameter determination in the fatigue residual strength degradation model is proposed. The new method and minimization technique is compared experimentally to account for the effect of tension-compression fatigue loading of spheroidal graphite cast iron and graphite/epoxy laminate. It is shown that the correlation between the experimental results and the theoretical prediction on the fatigue life and residual strength distribution using the proposed method is very reasonable. Therefore, the proposed method is more adjustable in the determination of the parameter than minimization technique for the prediction of the fatigue characteristics.

• 콘크리트학회논문집
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• 제16권1호
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• pp.27-35
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• 2004

지금까지 콘크리트에 대한 피로실험과 연구는 대부분 압축응력, 휨응력을 받는 경우에 대하여 연구를 진행하였으나 실제 교량이나 도로 포장콘크리트 구조물은 이축응력상태의 조합응력을 받게 된다. 따라서, 본 연구에서는 이러한 콘크리트 구조체가 받게 되는 이축응력 상태를 이상적으로 재현할 수 있는 쪼갬인장 피로실험방법을 제안하고 적용성을 평가 하고자 하였다. 실험은 ${\phi}15{\times}30cm$를 사용한 KS 규정을 응용하여 ${\phi}15{\times}7.5cm$의 시편을 제작하고, 쪼갬인장 피로실험에 적용하기 위한 타당성 검증을 수행하였으며, 이상적 탄성재료인 강재와 고체의 비교를 위하여 모르타르 시편을 제작하여 검증실험을 수행하였다. 또한, 이론적 고찰과 유한요소 해석을 수행하여 이론치와 해석치의 비교 고찰하였으며 정적 강도측정 및 게이지 부착실험을 수행하여 타당성을 입증하고자 하였다. 실험결과, FEA결과, 수평응력과 압축응력의 비는 3.1로 나타나 이론치 3.0과 유사한 결과를 얻을 수 있었다. 수평응력은 시편의 길이가 30cm일 경우 이론상 3MPa이지만, 본 연구에서는 시편의 길이가 30cm와 5cm일 때 각각 2.98MPa와 2.96MPa로 나타났다. 쪼갬인장 피로실험방법은 유한요소 해석, 정적 강도측정 및 게이지 부착실험모두에서 충분한 타당성을 나타내었으며, 이 방법은 실제 응력 모사, 실험의 간편성, 현장 시편 이용 가능성 등 많은 장점을 가지고 있는 것으로 판단되어 향후 교량이나 도로포장 구조물에 사용되는 콘크리트의 피로거동을 모사하는데 적합한 실험방법으로 사료된다.

• 한국소성가공학회:학술대회논문집
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• 한국소성가공학회 2005년도 추계학술대회 논문집
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• pp.193-197
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• 2005

Influences of microstructure on high-cycle fatigue (HCF) limit of high carbon $(>0.7wt.\;\%)$ steel filaments used for tires have been investigated. A series of the fatigue tests was carried out depending on carbon content by using Hunter-type tester at a frequency of 60 Hz at a tension/compression stress of 900 to 1500 MPa. Microstructural changes of the filaments were identified in the lateral direction by using transmission electron microscopy (TEM). It was found that the mechanical properties, such as fatigue limit and tensile strength, were improved with increasing carbon content, which was mainly attributed to decreased lamellar spacing and cementite thickness. However, the fatigue ratio, which is defined as the ratio of the fatigue limit to the tensile strength, was reduced in a higher carbon range of 0.8 to $0.9\;wt.\%$, while the fatigue ratio was nearly constant in a lower carbon range of 0.7 to $0.8\;wt.\%$. Overall mechanical properties of the filaments, depending on carbon content, have been discussed in terms of the microstructural parameter change of lamellar spacing and cementite thickness. In addition, the variation of cementite morphology on the fatigue crack propagation of high carbon $(0.9wt.\;\%)$ filaments will be discussed.