• Journal of the Korean Society for Nondestructive Testing
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• v.26 no.5
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• pp.315-320
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• 2006

This paper describes stress analysis and fatigue limit evaluation of plate with V-notch and hole-notch by lock-in infrared thermography. Temperature variation of a specimen under cyclic loading is negatively proportional to the sum of principle stress change and the surface temperature measured by infrared camera is calculated to the stress of notch specimens, based on thermoelastic equation. And also, fatigue limitation can be evaluated by the change of intrinsic energy dissipation. Fatigue limitation of two notch specimens is evaluated as 164 MPa and 185 MPa, respectively and the stress measured by Lock-in infrared Thermography show good agreement within 10% error.

• Composites Research
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• v.30 no.2
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• pp.149-157
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• 2017

In this paper, fracture behavior of laminated composites with notch was studied by cohesive zone modeling approach. The numerical modeling proceeded by first generating 3 dimensional solid element meshes for notched laminated composite coupon configurations. Then cohesive elements representing failure modes of fiber fracture, matrix cracking and delamination were inserted between bulk elements in all regions where the corresponding failures were likely to occur. Next, progressive failure analyses were performed simulating uniaxial tensile tests. The numerical results were compared to those by experiment available in the literature for verification of the analysis approach. Finally, notched laminated composite configurations with selected stacking sequences were analyzed and the failure behavior was carefully examined focusing on the failure initiation and progression and the dominating failure modes.

• Journal of the Korea Institute of Information and Communication Engineering
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• v.8 no.8
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• pp.1700-1704
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• 2004

In this paper a novel power converter for some notches generation in the point of common coupling is described. The magnitude, width, polarity, and position of the notches generated by the proposed scheme can be varied arbitrary with simple control. The scheme has good features of simple structure, high reliability, low cost, high efficiency, and the capability of arbitrary several notches generation. The converter can be used for the test of custom power devices such as UPS, DVR, active power filter, etc. The circuit operation is described and the usefulness of the scheme is verified through simulations.

• Composites Research
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• v.23 no.3
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• pp.1-6
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• 2010

Recently, CFRP composite is more and more used in the various fields because of a higher specific modulus, chemical property and so on. Most products using CFRP composite are manufactured by construction of components. Various components are joined with those by bolts and pins. Holes for bolts and pins decrease strength and fatigue life of components, because those act as notch in structures. In this paper, we experimentally evaluated the fatigue life of hole-notched and unnotched weave CFRP plate. Then, we compared the two results and proposed an equation for prediction of fatigue life.

• Tunnel and Underground Space
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• v.19 no.4
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• pp.366-372
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• 2009

Recently, in order to achieve smooth fracture plane and minimize the excavation damage zone in rock blasting, controlled blasting methods which utilize new technologies such as electronic delay detonator (EDD) and a notched charge hole have been suggested. In this study, smooth blastings utilizing three wing type notched charge holes are simulated to investigate the influence of explosive initial density on the resultant fracture plane and damage zone using dynamic fracture process analysis (DFPA) code. Finally, based on the dynamic fracture process analyses, novel smooth blasting method, ED-Notch SB (Electronic Detonator Notched Charge Hole Smooth Blasting) is suggested.

• Journal of Power System Engineering
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• v.6 no.1
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• pp.61-67
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• 2002

15Cr-5Ni 석출강화 스테인리스강 3종류의 피로균열 발생과 성장 특성 및 파괴인성에 대하여 노치함수로서 연구하였다. 3종류강의 열처리 조건은 $482\;^{\circ}C,\;579\;^{\circ}C$ 및 $621\;^{\circ}C$이다. $621\;^{\circ}C$에서 4시간동안 열처리한 시험편 C는 약 $280\;MPa\;\sqrt{m}$의 가장 높은 파괴인성을 보였으며, 3종류에서 피로균열 성장이 가장 늦었다. $482\;^{\circ}C$에서 1시간 열처리한 시험편 A에서, 피로균열발생한계, ${\Delta}k{\rho}$, 는 노치반경0.3 mm에서 약 $280\;MPa\;\sqrt{m}$의 가장 높은 값을 보였다. 시험편 A는 시험편 B와 C보다 피로균열 성장이 빨랐지만, 피로균열 발생이 늦었다. 예 하중에 의한 노치선단의 압축잔류응력은 노치 시험편의 피로강도 향상에 유용한 방법이었다.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2003.06a
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• pp.1358-1361
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• 2003

In this study, intrinsic static/dynamic fracture toughness of Al 7175-T74 are evaluated from the apparent static/dynamic toughness of notched specimen. The notch/crack critical average stress fracture model is suggested to establish the relationship to predict the intrinsic fracture toughness from the apparent fracture toughness of a notched specimen. The notch/crack critical average stress fracture model is established using the relation between the notch root radius and the effective distance calculated by finite element analysis. It is conclude that the true fracture toughness can be estimated from test results of apparent fracture toughness measured by using a notched specimen. Also, critical notch root radius can be predicted by notch/crack critical average stress fracture model.

• Aerospace Engineering and Technology
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• v.1 no.2
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• pp.75-82
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• 2002

This paper presents a summary of the input data, requirements and notch prediction analysis for sinusoidal excitation test of a satellite. In the notch prediction analysis, the loads at excitation points and internal loads at the important locations on satellite structure were obtained. After checking of limit loads and margin of safety for each location, the notched sinusoidal test inputs were generated using the results of the notch prediction analysis.

• Proceedings of the Korean Nuclear Society Conference
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• 1996.11b
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• pp.557-562
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• 1996

조사전 및 감시시험시 용접열영향부(heat affected zone, HAZ)의 인성평가를 위해 제작되는 샤피(Charpy) 충격시험편의 노치(notch) 위치에 대하여 현재의 규정에 대한 타당성을 검토하였다. 적용규정은 HAZ 시험편의 노치위치를 용접용융선(fusion line, FL) ＋ 모재측 0.8 mm 로 제한하고 있다. 그러나, 본 연구결과, 이 부위는 다층(multipass) 용접시 후속열이력에 의해 결정립이 미세화되어, 인장강도와 경도 및 충격인성이 모재나 용접부에 비하여 양호하게 나타났다. 한편, FL ＋ 4 mm 이상의 다른 위치에서는 강도와 경도 및 충격인성이 모두 모재와 용접부에 비하여 낮은 값을 보였다. 이는 다층용접에 의한 후속열이력 및 용접후열처리(post weld heat treatment, PWHT)에 의해 금속조직학적 영향을 받은 것으로 판단되었다. 일련의 시험결과로부터, 조 사전 및 감시시험용 샤피충격시험편의 HAZ 에 있어서의 노치위치에 대한 현재의 규정을 재검토할 필요가 있음을 제안하였다.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2003.10a
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• pp.233-233
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• 2003