• 한국자동차공학회논문집
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• 제14권1호
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• pp.79-85
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• 2006

CFRP(Carbon Fiber Reinforced Plastics) of the advanced composite materials as structural materials for vehicle, has a wide application in light-weigh structural materials of airplanes, ships and automobiles because of high strength and stiffness, However, there is a design variable to be considered in practical application of the laminate composite materials, these materials are vulnerable to transverse impact. This paper is to study the effects of stacking sequence and curvature on the penetration characteristics of composite laminate shell. They are stacked to $[0_3/90_3]S,\;[90_3/0_3]s\;and\;[0_2/90_3/0]s,\;[90_2/0_3/90]s$ and their interlaminar number two and four. They are manufactured to various curvature radius (R=100, 150, 200mm and $\infty$), When the specimen is subjected to transverse impact by a steel ball, the velocity of the steel ball was measured both before and after impact by determing the time for it to pass two ballistics-screen sensors located a known distance apart. The critical penetration energy of specimen A and B with less interfaces were a little higher than those of C and D. As the curvature increases, the critical penetration energy increases linearly because the resistance to the in-plane deformation as well as bending deformation increases, which need higher critical penetration energy. The specimen A and C have higher critical penetration energy than B and D because of different stacking sequences. We examined crack length through a penetration test. For the specimen A with 2interfaces, the longest circumferential direction crack length were observed on the first interface from the impact point. For the specimen B 4-interface, the longest circumferential direction crack length were observed on the second interface from the impact point.

• Steel and Composite Structures
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• 제43권1호
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• pp.19-30
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• 2022

The static strength and fatigue crack resistance of the aircraft skin structures depend on the materials used and joint type. Most of the commercial aircraft's skin panel structures are made from aluminium alloy and carbon fibre reinforced epoxy. In this study, the fatigue resistance of four joint configurations (metal/metal, metal/composite, composite/composite and composite/metal) with riveted, adhesive bonded, and hybrid joining techniques are investigated with experiments and finite element analysis. The fatigue tests were tension-tension because of the typical nature of the loads on aircraft skin panels susceptible of experimenting fatigue. Experiment results suggest that the fatigue life of hybrid joints is superior to adhesive bonded joints, and these in turn much better than conventional riveted joints. Thanks to the fact that, for hybrid joints, the adhesive bond provides better load distribution and ensures load-carrying capacity in the event of premature adhesive failure while rivets induce compressive residual stresses in the joint. Results from FE tool ABAQUS analysis for adhesive bonded and hybrid joints agrees with the experiments. From the analysis, the energy release rate for adhesive bonded joints is higher than that of hybrid joints in both opening (mode I) and shear direction (mode II). Most joints show higher energy release rate in mode II. This indicates that the joints experience fatigue crack in the shear direction, which is responsible for crack opening.

• Journal of Mechanical Science and Technology
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• 제16권8호
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• pp.1064-1071
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• 2002

Stainless steel pipe of type 304 the with a wall thickness of 26.9 mm and the outer diameter 406.4 mm is welded by manual arc welding process. Mechanical properties and fracture toughness of type 304 stainless steel are investigated in the temperature ranging from room temperature to -162$^{\circ}C$ The results obtained are summarized as follows. The tensile strength noticeably increases as the temperature becomes lower while the yield strength is relatively insensitive to temperature. The Charpy impact energy and CTOD values become higher in the case that crack propagation direction is aligned to the transverse axis upon the rolling direction than longitudinal direction. The drop of fracture toughness is associated with the noticeable diminution of plastic component as temperature seduces from room temperature to -162$^{\circ}C$ .

• 한국측량학회지
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• 제23권1호
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• pp.9-17
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• 2005

본 연구는 디지털 비디오카메라를 이용하여 아스팔트 콘크리트 포장의 노면을 촬영하고 획득된 영상을 분석함으로써, 대상 도로노면의 정보를 추출하는데 그 목적이 있다. 먼저, 수치영상처리에 의한 도로노면정보의 정확도를 분석하기 위해 기준점 측량에 의한 성과와 비교·분석하였다. 그 결과, X방향으로 0.0427m, Y방향으로 0.0527m, Z방향으로 0.1539m의 평균오차를 나타내었으며, 이는 축척 1/1,000 이하의 지도제작 및 GIS 자료로 충분히 활용성이 있는 것으로 판단된다. 또한, 처리된 수치영상을 분석하여 도로노면의 평가를 위한 중요 요소인 균열률, 소성변형량, 그리고 종단평탄성 정보를 획득할 수가 있었으며, 이를 이용하여 공용성지수와 유지관리지수를 산출함으로써, 대상도로의 노면평가를 수행할 수가 있었다. 향후 도로를 대상으로 취득된 양질의 영상정보를 축적함으로 인해 포장유지관리시스템 분야에 있어서 중요한 기초 자료를 제공할 수 있을 것으로 기대된다.

• Structural Engineering and Mechanics
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• 제66권5호
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• pp.569-582
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• 2018

Effects of crack separation, bridge area, on the tensile behaviour of concrete are studied experimentally and numerically through the Brazilian tensile test. The physical data obtained from the Brazilian tests are used to calibrate the two-dimensional particle flow code based on discrete element method (DEM). Then some specially designed Brazilian disc specimens containing two parallel cracks are used to perform the physical tests in the laboratory and numerically simulated to make the suitable numerical models to be tested. The experimental and numerical results of the Brazilian disc specimens are compared to conclude the validity and applicability of these models used in this research. Validation of the simulated models can be easily checked with the results of Brazilian tests performed on non-persistent cracked physical models. The Brazilian discs used in this work have a diameter of 54 mm and contain two parallel centred cracks ($90^{\circ}$ to the horizontal) loaded indirectly under the compressive line loading. The lengths of cracks are considered as; 10 mm, 20 mm, 30 mm and 40 mm, respectively. The visually observed failure process gained through numerical Brazilian tests are found to be very similar to those obtained through the experimental tests. The fracture patterns demonstrated by DEM simulations are mostly affected by the crack separation but the tensile strength of bridge area is related to the fracture pattern and failure mechanism of the testing samples. It has also been shown that when the crack lengths are less than 30 mm, the tensile cracks may initiate from the cracks tips and propagate parallel to loading direction till coalesce with the other cracks tips while when the cracks lengths are more than 30 mm, these tensile cracks may propagate through the intact concrete itself rather than that of the bridge area.

• 대한기계학회논문집
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• 제9권2호
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• pp.150-157
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• 1985

본 연구에서는 자연적인 미소흠함주위에 발생, 전파하는 피로크랙의 거동을 검토하기 위하여, 기존재료가 갖고 있는 흠함이나 비금속개재물을 대신할 수 있다고 생각되는 크기가 다른 비관통 인공미성구멍을 갖는 여러 종류의 시험편을 준비하고, 이 시험편들이 갖는 인공미성구멍주위에 발생전파하는 피로크랙의 거동을, 금속현미경 관찰을 토대로 상세히 고찰하였다. 그리고 이러한 관찰을 기초로 하여 비관통인공미 성구멍의 대성에 따른 피로한계도거동에 대해서도 고찰하였다.

• 한국지반공학회:학술대회논문집
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• 한국지반공학회 1988년도 학술세미나 강연집
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• pp.3-67
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• 1988

Model studies on the response of homgeneous earth embankment dams subjected to strike-slip fault movement have been penomed via centrifuge and finite element analysis. The centrifuge model tests have shown that crack development in earth embankment experiences two major patters: shear failure deep inside the embankment and tension failure near the surface. The shear rupture zone develops from the base level and propagates upward continuously in the transverse direction but allows no open leakage chnnel. The open tensile cracks develop near the surface of the embankment, but they disappear deep in the embankment. The functional relationship has been developed based on the results of the centrifuge model tests incorporating tile variables of amount of fault movement, embankment geometry, and crack propagation extent in earth des. This set of information can be used as a guide line to evaluate a "transient" safety of the duaged embankment subjected to strike-slip fault movement. The finite element analysis has supplemented the additional expluations on crack development behavior identified from the results of the centrifuge model tests. The bounding surface time-independent plasticity soil model was employed in the numerical analysis. Due to the assumption of continuum in the current version of the 3-D FEM code, the prediction of the soil structure response beyond the failure condition was not quantitatively accurate. However, the fundamental mechanism of crack development was qualitatively evaluated based on the stress analysis for the deformed soil elements of the damaged earth embankment. The tensile failure zone is identified when the minor principal stress of the deformed soil elements less than zero. The shear failure zone is identified when the stress state of the deformed soil elements is at the point where the critical state line intersects the bounding surface.g surface.

• 한국컴퓨터정보학회논문지
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• 제12권2호
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• pp.77-82
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• 2007

본 논문에서는 콘크리트 표면 균열의 방향성을 효율적으로 인식하기 위하여 영상처리 기법을 적용하여 균열을 자동으로 검출하고 개선된 Max-Min 신경망을 제안하여 균열의 방향성을 자동으로 인식하는 기법을 제안한다. 균열 영상에서 빛의 영향을 효율적으로 보정하기 위해 모폴로지 기법인 채움 연산을 적용하고 Sobel 마스크를 적용하여 균열의 에지를 추출한 후, 반복 이진화를 적용하여 균열 영상을 이진화한다. 이진화된 균열 영상에서 2차례에 걸쳐 잡음 제거 연산을 수행한 후, 균열을 추출한다. 본 논문에서는 Max-Min 신경망을 개선하여 추출된 균열의 방향성을 자동으로 인식한다. 개선된 Max-Min 신경망은 delta-bar-delta 알고리즘을 적용하여 학습률을 자동으로 조정한다. 실제 콘크리트 표면 균열 영상을 대상으로 실험한 결과, 개선된 Max-Min 신경망이 균열의 방향성 인식에 효율적임을 확인하였다.

• 한국지반공학회논문집
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• 제19권2호
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• pp.171-178
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• 2003

날개크랙과 이차크랙은 암석의 일축압축 및 이축압축 조건에서 관측되는 특정한 형태의 크랙이다. 본 연구에서는 석고로 제작된 실험체내에 발생하는 날개크랙과 이차크랙의 형태적 측면을 미시적 및 거시적 관점에서 관측하였다. 날개크랙의 진행방향을 따라 미소인장크랙이 관측되었으며 미소인장크랙은 공극간의 연결과 분지현상을 통하여 진전되었다. 날개크랙의 개시점에서 다중의 미소인장크랙의 개시가 관측되었으며 미소인장크랙은 굴곡진 진행을 보인다. 또한 이차크랙과는 달리 미소인장크랙은 상대적으로 일정한 크랙의 틈을 보이며 인장에 의한 할렬파괴에 의해 진행되는 것으로 나타났다. 이차크랙의 미시적 관측에서는 미소파쇄대가 관측되었다. 이차크랙의 파괴구간 내에서는 입자 및 집괴의 분리, 경사진 미소파쇄대의 형성 및 불규칙한 크기의 틈을 가진 미소파쇄대가 관측되었다. 이러한 결과는 이차크랙이 전단에 의해 형성됨을 보이고 있다 날개크랙과 이차크랙은 서로 다른 크기의 파괴진행구간을 보이고 있으며 각각의 크랙의 진행 방향에 직각방향으로 측정된 파괴진행구간의 폭은 날개크랙의 경우 10$\mu{m}$에서 20$\mu{m}$ 정도이며 이차크랙은 100$\mu{m}$에서 200$\mu{m}$ 정도이다.

• E2M - 전기 전자와 첨단 소재
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• 제10권6호
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• pp.519-527
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• 1997

The micro crack was occurred where the stress concentrated by the thermal stress which was induced during the cooling period after molding process or by the various reliability tests. In order to estimate the possibility of development from inside micro crack to outside fracture, the fracture toughness of EMC should be measured under the various applicable condition. But study was conducted very rarely for the above area. In order to provide a was to decide the fracture resistance of EMC (Epoxy Molding Compound) of plastic package which is produced by using transfer molding method, measuring fracture is studied. The specimens were made with various EMC material. The diverse combination of test conditions, such as different temperature, temperature /humidity conditions, different filler shapes, and post cure treatment, were tried to examine the effects of environmental condition on the fracture toughness. This study proposed a way which could improve the reliability of LOC(Lead On Chip) type package by comparing the measured $J_{IC}$ of EMC and the calculated J-integral value from FEM(Finite Element Method). The measured $K_{IC}$ value of EMC above glass transition temperature dropped sharply as the temperature increased. The $K_{IC}$ was observed to be higher before the post cure treatment than after the post cure treatment. The change of $J_{IC}$ was significant by time change. J-integral was calculated to have maximum value the angle of the direction of fracture at the lead tip was 0 degree in SOJ package and -30 degree in TSOP package. The results FEM simulation were well agreed with the results of measurement within 5% tolerance. The package crack was proved to be affected more by the structure than by the composing material of package. The structure and the composing material are the variables to reduce the package crack.ack.