• Journal of Ocean Engineering and Technology
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• v.6 no.2
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• pp.71-75
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• 1992

기구나 구조물의 피로수명은 노치에서의 피로균열 방생수명에 의하여 지배되기때문에 노치로 인한 피로강도감소계수 $K_f$는 피로설계상 대단히 중요한 인자이다. 노치 선단(Notch root)에서의 피로균열발생명수 N$_c$를 기준으로하면 탄성응력집중계수 $K_t$가 10 정도까지 $K_f$와 $K_t$간에는 거의 직선적인 관계가 있음이 이다- 고에 의하여 명석해졌으나 이는 인장,압축의 축력이 작용하였을 때이며 따라서 기구나 구조부재는 축력외에도 굽힘 피로 하중이 작용하였을때도 많으므로 본 연구에서는 굽힘 피로 하중을 받았을때도 있다. -고의 결론이 적용되는지는 검시코져 본 연구를 실시하였다.

• Journal of the Korean Society for Nondestructive Testing
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• v.30 no.2
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• pp.139-145
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• 2010

Bending fatigue of aluminium alloy was characterized by acoustic nonlinearity of narrow band laser-generated surface wave. The higher harmonic components generated intrinsically by arrayed line laser beam were analyzed theoretically and acoustic nonlinearity was measured successfully on the surface of fatigue damaged aluminium 6061 alloy. The acoustic nonlinearity increased as a function of fatigue cycles and has close relation with damage level. Consequently, the nonlinear acoustic technique of laser-generated surface wave could be potential to characterize surface damages subjected to fatigue.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.38 no.10
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• pp.1163-1169
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• 2014

In this study, a fatigue assessment method for vehicle suspension systems having welded geometries was established under a bending loading condition. For the fatigue life estimation of the actual product's welded joints made of different steels, bending fatigue tests were performed on welded specimens with a simplified shape for obtaining the moment-fatigue-life plot. Further, geometry modeling of the simplified welded specimens was conducted. Results of finite element analysis were used to obtain the stress-fatigue-life plot. The analysis results were also used to calculate the stress concentration factors for notch-factor-based fatigue life estimation. The test results were compared with results of the general notch-factor-based fatigue life estimation for improving fatigue assessment. As a result, it was concluded that both the welded fatigue tests and the notch-factor-based fatigue life estimation are necessary for accurate fatigue assessment.

• Journal of the Korean Institute of Gas
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• v.3 no.3 s.8
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• pp.1-8
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• 1999

Three-point bending fatigue properties of austenitic 304 stainless steel sheets were investigated at room temperature and LNG temperature($-162^{\circ}C$) in the strain range from 0.43 to $1.7\%$. The fatigue properties at $-162^{\circ}C$ were superior to those at room temperature due to the higher volume fractions of deformation-induced martensite. The cyclic hardening behavior owing to the deformation- induced martensite transformation was detected in both specimens. In room temperature testing, the mean load amplitude increased steadily with cycles, meaning that cumulative plastic incubation strain was required for martensite transformation. On the contrary, in $-162^{\circ}C$ tested specimen, the mean load amplitude increased rapidly within a few cycles due to the rapid transformation of martensite, and slightly decreased after the maximum is reached probably due to dynamic recovery.

• Journal of the Korean Society for Nondestructive Testing
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• v.28 no.4
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• pp.323-330
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• 2008

High cycle bending fatigue of socket welded small bore pipe was characterized, and also the fatigue crack initiation of small bore pipe was monitored in situ by the acoustic emission (AE) technique. The STS 316L stainless steel specimens were prepared by gas tungsten arc welding (GTAW) process having the artificial defect (i.e., lack of penetration) and defect free at the root. The fatigue failure was occurred at the loc for high stress and root for relatively low stress. The crack initiation cycles ($N_i$) was defined to the abrupt increase in AE counts during the fatigue test, and then the cracks were observed by the radiographic test and electron microscope before and after the fatigue crack initiation cycles. The socket welded pipe damaged by bending fatigue was studied regarding the welding defect, failure mode, and crack initiation cycles for the diagnosis and monitoring.

• Proceedings of the KSME Conference
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• 2005.11a
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• pp.176.1-176.1
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• 2005

• Transactions of the Korean Society of Mechanical Engineers
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• v.13 no.1
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• pp.199-203
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• 1989

본 연구에서 제작된 시험기는 연구자 개인의 경제적 수준에서 충분이 제작이 가능한 것이다.

• Journal of the KSME
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• v.17 no.1
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• pp.32-39
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• 1977

파괴역할적으로 피로문제를 다룰 때는 언제나 crack의 존재를 전재로 한다. 재료가 피로하중을 받아 파괴에이르는 과정의 설명은, 일차적으로는 피로에의한 crack의 발생이고, 다음단계로는 발 생한 crack들의 상호연결 또는 성장을 거쳐 최종적으로 파단에 이른다는 순서로 이루어진다고 보 기 때문이다. 또한, crack의 존재를 전제로 하더래도 crack청단의 응력장이 탄성론적으로 해석될 수 있어야함도 절대적인 전제가 되고 있다. 모든 피로제엔 각경형태의 crack발생, 성장이 관찰되 고 있는데, 이들 모든 crack들이다. 파괴역학적으로 다루어 질 수 있는 것은 물론 아니고, 아직도 K해석이 도어있지 않은 crack들이 많이 남아 있는 것이다. 예컨대 회전굽힘 피로시험편에서 관찰 되는 각종 형태의 표면피로 crack들은 응력해석의 곤란 때문에 아직은 이들에 적용시킬 K의 표 식이 없는 실정이라 하겠다. 이들 crack에 대해서는 K해석 뿐만 아니고, 피로역학적인 다른 Factor 즉 $r_{p}$라든가 .phi.같은 것들도 이해색상태에 있어 이 분야에의 연구가 많이 기대되고 있는 실정이다. Crack에 대한 연구는, 그것이 파괴의 전제가 되기 때문에 큰 의의를 갖는다고 보 겠는데 표면 Crack이 연결 또는 성장해서 시편의 전주를 완전히 일주 했어도 그것만으로는 바로 재료의 파괴에 직결이 되지 않는 것도 이 시험편의 특색이라 하겠다. 물론 회전굽힘 피로시험편 외에도 K해석이 되어있지 않은 경우는 아직도 많으며, K가 해석되어 있는 경우에 대해서도 정확 한 경계조건 등을 잘 검토해 가면서 응용함이 옳을 것이다. 화전굽힘피로의 경우나 그밖의 예에 서와같이 정확한 K해석이 이루어져 있지 않드래도 연구자에 따라 "Effective Streess Intensity Factor"라는 것을 쓰는 예도 왕왕있는데, 이에는 상당한 검토와 타당성제가 요구되고 있으며, 그 사용가능성여부에 대해서는 논란이 많이 따르는데 상례이기도 하다. 몇가지의 피로구열해석예를 들어보기로 한다. 들어보기로 한다.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.36 no.10
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• pp.1227-1234
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• 2012

In this study, fatigue tests were carried out using real-scale pipe bend specimens with wall-thinning defects under a cyclic bending load together with a constant internal pressure of 10 MPa. The wall-thinning defect was located at the extrados and the intrados of the pipe bend specimens. A fully reversed cyclic in-plane bending displacement was applied to the specimens. For the pipe bends with wall thinning at the extrados, an axial crack occurred at the crown of the pipe bend rather than at the extrados where the defect was located. In addition, the fatigue life was longer than that of a sound pipe bend predicted from the design fatigue curve in ASME Sec.III, and it was less dependent on the axial length of the wall-thinning defect. For the pipe bends with wall thinning at the intrados, a circumferential crack occurred at the intrados. In this case, the fatigue life was much shorter than that of a sound pipe bend predicted from the design fatigue curve, and it clearly decreased with decreasing axial length of the wall-thinning defect.

• Journal of the Society of Naval Architects of Korea
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• v.29 no.1
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• pp.93-102
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• 1992

In this paper presented is the reliability analysis of a double skinned hull structure against the ultimate bending moment and fatigue strength under longitudinal bending. The ultimate bending strength is obtained through the beam-column approach in which the load-end shortening curves(stress-strain curves) of stiffened plates under mini-axial compression are derived using the concept of plastic hinge collapse. The fatigue damage only is considered as fatigue failure for which the Miner's damage rule is employed. Assessed are fatigue reliability for the possible joint types found at deck structure. Also included is the reliability analysis of a series system of which elements are ultimate and fatigue failure.