• Computational Structural Engineering
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• v.8 no.2
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• pp.95-102
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• 1995

해양구조물의 피로파괴 형태는 매우 다양하며 설계단계에서 구조요소의 피로수명 예측은 중요하다. 각가지 피로해석 방법에 대해서 연구가 활발히 진행되었으며 접근방법에 대한 논의도 활발한 연구와 함께 진행되었다. 본 논문에서는 피로해석 방법중 스펙트랄 방법과 그 구성요소에 대해서 연구되었으며 간략화된 피로해석 방법이 제시되었고 그 특성이 비교 검토되었다. 두가지 피로해석 방법의 장단점이 조사되었고 관련된 인자인 응력집중계수, 응력폭-수명 관계 곡선 또한 연구되었다. 전형적인 반 잠수식시추선의 브레이싱 부재의 피로수명 예측을 위하여 간략화된 피로해석 방법과 스펙트랄 피로해석 방법이 작용되었으며 이를 통하여 두 방법의 유용성이 확인되었다. 또한 간략화된 피로해석 방법을 이용한 민감도 해석이 수행되었다. 본 논문에서 수행된 피로해석 결과는 스펙트랄 피로해석 방법이 보다 현실적인 피로수명 예측을 할 수 있는 방법이라는 사실을 보여주었다.

• Journal of the Korean Society for Aviation and Aeronautics
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• v.19 no.1
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• pp.15-23
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• 2011

The purpose of this paper is to investigate the time behavior of a multiple crack problems. It is assumed that the medium contains cracks perpendicular to the crack surfaces, that the thermo-mechanical properties are continuous functions of the thickness coordinate. we use the laminated composite plate model to simulate the material non-homogeneity. By utilizing the Laplace transform and Fourier transform techniques, the multiple crack problems in the non-homogeneous medium is formulated. Singular integral equations are derived and solved to investigate the multiple crack problems. As a numerical illustration, transient thermal stress intensity factors(TSIFs) for a functionally graded material plate subjected to sudden heating on its boundary are provided. The variation in the TSIFs due to the change in material gradient and the crack position is studied.

• Journal of Ocean Engineering and Technology
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• v.2 no.1
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• pp.106-115
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• 1988

반잠수식 시추선의 설계에 있어서 구조의 피로수명을 정확하게 추정하는 것은 매우 중요하며, 또한 어려운 일이다. 본 논문에서는 이미 실용화된 Aker H-3모델에 대하여 Palmgren-Miner 가정에 의하여 시추선의 hot-point인 수평 및 수직 K-brace 멤버에 대하여 피로수명을 로이드 선급의 커브에 따라 계산한 결과 북해의 해성환경 조건에서는 16년 동안 계속 작업을 할 수 있다는 결론을 얻었으나 응력 집중계수 (SCF)를 선정하는데 불확실성으로 인하여 사용하는데 주위를 요한다.

• Tunnel and Underground Space
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• v.30 no.5
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• pp.473-483
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• 2020

This paper examines the vertical stress change concentrated on mine pillar which occurs due to the stress disturbance from opening excavation at room and pillar mine by FLAC3D, a finite difference method (FDM) software. The mesh size combination is decided with a careful consideration of relative error and run-time, then its performance is verified. A series of numerical analyses is conducted and the vertical stress at central pillar was observed for the test cases of 1×1 to 11×11 mine pillars, 40 m to 320 m depth with 40 m difference. The results show that the vertical stress of pillar approaches to the similar value with the value estimated by tributary area theory(TAT) when the development area (N_P) is increased or the height of overburden (H_OB) is decreased, while it is overestimated in the opposite case. Furthermore, it also represents that the vertical stress factor (VSF) converges to a specific value when the depth is increased whille keeping the development area identical.

• Composites Research
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• v.28 no.1
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• pp.6-14
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• 2015

Polymerization shrinkage stress analysis of dimethacrylate-based composite (Clearfil AP-X, Kuraray) and silorane-based composite (Filtek P90, 3M ESPE) used for dental composite restorations was performed using strain-gage measurement and FEM analysis. A theoretical equation based on Young's modulus and polymerization shrinkage of the composite resin was proposed to predict the polymerization shrinkage stress. Experimental results showed that the maximum shrinkage stress of Clearfil AP-X was about 2.8 times higher than Filtek P90. FEM analysis agreed with such experimental stress behaviours and showed that the maximum Von-Mises stress appeared near the margin of the filled resin adhered with PMMA ring. The stress concentration at the interface on the specimen surface was higher than that in the interior. The maximum error of shrinkage stress by the theoretical equation was reasonable within 5% in comparison to FEM results under plane stress.

• Journal of the KSME
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• v.29 no.2
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• pp.118-124
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• 1989

피로파괴의 발생원인을 살펴보면 다음과 같이 4가지로 구별된다. (1) 설계불량 (2) 가공불량 (3) 소재불량 (4) 부적절한 사용 그러나 현재 기계설계시 일반적으로 형상계수 및 충격계수를 포함한 안전율을 여유있게 고려하기 때문에 피로강도가 간접적으로 설계시 반영되어 피로파괴는 주로 가공이나 원소재 불량 및 사용상의 부주의에 의한 경우가 대부분이다. 즉 기계가공 도중에 노치가 유입되어 응력집중을 발생시키거나, 규정된 표면처리 혹은 열처리가 이루어지지 못해서 재료의 피로강도가 저하한 경우가 많으며, 소재 역시 비금속 개재물이 다량 함유되어 있거나 열처리 특성이 조악한 소재가 사용되어 요구되는 강도를 확보하지 못한 경우도 많다. 그 반면 사용자 측에서도 설계강도를 무시한 과부하를 인가하거나, 부식환경 혹은 고온에서 사용하여 피로파괴를 촉진시키는 경우도 있으므로 사용자도 설계조건을 인식하여 그 한계를 넘지 않도록 해야 한다. 피로파괴는 단순한 원인에 의한 경우가 적고 복잡한 여러 형상이 중첩되는 경우가 많기 때문에 해석하기 어려운 경우가 많다. 결국 피로 파괴의 방지는 피로강도를 저하시킬 수 있는 요인들을 종합하여 설계단계에서부터 최종 사용단계까지 지속적인 관리에 의해서만 달성 될 수 있다.

• Journal of the Korean Society for Railway
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• v.7 no.2
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• pp.125-129
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• 2004

This study investigates the fatigue lift estimation of butt weld specimen for the railway vehicle by examining butt weld bead profiles. The butt weld beads, which are welded by semi-robot method, have non-uniform bead profiles described by $\theta$, p and h. The stress concentration factors, K$\_$t/, are changed by different $\theta$, p and h from 1.395 to 2.863. Hence, the sensitivity of K$\_$k/ is changed by each $\theta$, p and h. As $\theta$ becomes lower and p and h become higher, K$\_$t/ increases. The fatigue life can be estimated very closely for the AAY specimens without residual stress using only butt weld bead profiles. But, for the AAN specimens with residual stress, the fatigue life must be estimated by considering both the weld bead profiles and the residual stress data.

• Journal of Welding and Joining
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• v.16 no.4
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• pp.73-82
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• 1998

This paper is especially concerned with the weldment between support beam and square bar that plays important roles in control box of Expansion Joint as a brdige structure. Fatigue strength ({TEX}$$\sigma$_{ult}${/TEX}) of the weldment is dependent on notch factor ({TEX}$K_{f}${/TEX}) become important factors to predict fatigue life. The fatigue notch sensitivity (η) for metals can be divided into two types ; high and low notch sensitivity. In this work, the Expansion Joint weldment was found to have low notch sensitivity. The maximum strain distribution during static loading is similar to the FEM analysis. Fatigue test of real structure was performed up to {TEX}$10^{6}${/TEX} cycles to be compared with predicted endurance limit.

• Journal of the Microelectronics and Packaging Society
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• v.19 no.2
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• pp.7-15
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• 2012

Semiconductor packages are increasingly moving toward miniaturization, lighter and multi-functions for mobile application, which requires highly integrated multi-stack package. To meet the industrial demand, the package and silicon chip become thinner, and ultra-thin packages will show serious reliability problems such as warpage, crack and other failures. These problems are mainly caused by the mismatch of various package materials and geometric dimensions. In this study we perform the numerical analysis of the warpage deformation and thermal stress of 4-layer stacked FBGA package after EMC molding and reflow process, respectively. After EMC molding and reflow process, the package exhibits the different warpage characteristics due to the temperature-dependent material properties. Key material properties which affect the warpage of package are investigated such as the elastic moduli and CTEs of EMC and PCB. It is found that CTE of EMC material is the dominant factor which controls the warpage. The results of RSM optimization of the material properties demonstrate that warpage can be reduced by $28{\mu}m$. As the silicon die becomes thinner, the maximum stress of each die is increased. In particular, the stress of the top die is substantially increased at the outer edge of the die. This stress concentration will lead to the failure of the package. Therefore, proper selection of package material and structural design are essential for the ultra-thin die packages.

• Journal of Korean Society of Steel Construction
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• v.18 no.2
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• pp.203-211
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• 2006

This paper presents a new, effective torsional constant for thin-waled open beams under concentrated and uniformly distributed torques. The proposed constant can be used directly, instead of the St. Venant torsional constant, for any generic comemrcial finite-element program, without modifying the algorithm. The derived torsional constant accounts for both the pure torsion and the warping torsion, and is equal to the St. Venant torsion constant times a correction factor. It is also shown, in the case of the St. Venant torsion, that the derived constant is identical to the torsional constant. The derived effective torsional constant is different from the one given by Elhelbawey et al. The pure torsional shear stress, the warping shear stress, and the warping normal stress were also determine d, using the maximum twisting angle. The accuracy of the proposed torsional constant was validated by comparing the numerical results with the closed-form solutions or other numerical results available in the literature.