• 한국지반환경공학회 논문집
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• 제15권2호
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• pp.5-15
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• 2014

목표신뢰도지수는 한계상태설계법에서 안전여유의 지표가 되며, 부분계수를 결정하는데 있어 매우 중요한 역할을 한다. 본 연구에서는 한계상태설계법에서 필요로 하는 목표신뢰도지수의 결정을 위하여 쇄석다짐말뚝이 적용된 6개소의 설계-시공사례를 조사하였다. 쇄석다짐말뚝의 주요 파괴모드인 팽창파괴에 대한 한계상태함수를 정의하고, 일계신뢰성해석법(FORM)을 이용하여 극한지지력, 이론식별, 신뢰도수준을 평가하였다. 현행 쇄석다짐말뚝의 신뢰도지수는 허용응력설계법에 의해 산정된 안전율과 비례하는 경향을 보였으며, 평균 신뢰도지수는${\beta}$=2.30으로 평가되었다. 신뢰성해석에 의해 평가된 신뢰도 수준과 기존 구조물 기초에 대한 목표신뢰도지수를 비교 분석한바, 쇄석다짐말뚝 기초는 말뚝기초 및 얕은기초에 비하여 비교적 낮은 안정성 수준이 요구되며, 쇄석다짐말뚝의 현재 신뢰도수준은 보강토옹벽, 쏘일네일링에서 제안된 목표신뢰도지수와 유사한 범위를 보이므로 쇄석다짐말뚝의 목표신뢰도지수를 ${\beta}_T$= 2.33으로 제안하였다.

• Journal of the Korean Wood Science and Technology
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• 제36권3호
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• pp.1-8
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• 2008

볼트 간격에 따른 국내산 낙엽송 집성재 이중 볼트접합부의 내력성능을 검토하기 위하여 휨 type 전단강도실험을 실시하였다. 전단시편은 강판삽입형 볼트접합부 시편으로서 볼트구멍은 볼트직경(12 mm, 16 mm), 볼트 개수(단일 볼트 : Control, 이중 볼트), 볼트 열 방향(섬유평행 : Type-A, 섬유직교 : Type-B) 그리고 볼트 간격(Type-A : 4 d, 7 d, Type-B : 3 d, 5 d)을 달리하여 제작하였다. 조건에 따른 볼트접합부의 강도성능과 파괴형상을 비교, 검토하였다. 설계표준(KBCS, 2000)시 볼트간격이 감소된 기준허용전단내력에 대한 저감계수를 산출하였다. 본 연구의 결과는 다음과 같다. 1) 단일 볼트접합부와 Type-A의 이중 볼트접합부의 볼트 한 개당 지압응력은 볼트의 직경, 볼트 간격과 비례 관계를 보여주었다. Type-B의 지압응력은 볼트의 직경이 증가할 때 감소하였고, 볼트 간격이 증가할 때 2~10% 정도 감소하였다. 2) 단일 볼트접합부와 Type-A의 이중 볼트접합부의 파괴형상은 연단거리 방향으로 할렬파단이 일어났다. Type-B의 경우 볼트간격이 3 d일 때 인장부위 볼트가 압축부위 볼트보다 더 굴곡되었고 인장부위볼트에서 할렬파단이 시작되었다. 5 d 시편의 경우 인장부위와 압축부위 볼트의 굴곡은 비슷하게 나타났으며, 압축부위볼트에서 할렬파단이 시작되었다. 3) 설계표준시 기준볼트 간격(Type A : 7 d, Type B : 5 d)에 따른 항복하중을 무차원화시켜 저감계수를 산출하였다. 12 mm 볼트접합부의 경우 Type-A인 볼트 간격 4d와 단일 볼트접합부의 저감계수는 각각 0.87, 0.55였고 Type-B인 볼트 간격 3 d와 단일 볼트접합부의 저감계수는 0.91, 0.55였다. 16 mm 볼트접합부의 경우 Type-A인 볼트 간격 4 d와 단일 볼트접합부의 저감계수는 0.96, 0.76이었고 Type-B인 볼트 간격 3 d, 단일 볼트접합부의 저감계수는 0.91, 0.77이었다.

• Earthquakes and Structures
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• 제12권1호
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• pp.79-89
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• 2017

As a new type of energy dissipation component with excellent mechanical performance, the Buckling-Retrained Braces (BRBs) were gradually applied in retrofitting and improving seismic performance of reinforced concrete structures in China. In order to investigate the seismic performance of reinforced concrete structures retrofitted with BRBs, quasi-static test of two single-bay and 3-story reinforced concrete frames specimens was conducted and introduced in this paper. Two 1/2 scaled specimens were designed to reflect real prototype structure. For comparison, one control specimen was designed without BRBs, and the other specimen was retrofitted with BRBs. And particularly, for the specimen retrofitted with BRBs, the BRBs were eccentric layout instead of usually concentric or x-shaped layout, aiming to be more suitable for large-span frames. In the test, the failure mode, carrying capacity, deformability, ductility and energy dissipation ability of both two specimens were investigated. Based on the test results of the measured hysterical curves, skeleton curves, the seismic performances such as bearing capacity, plastic deformability, energy dissipation ability and ductility of two specimens were fully studied. And from the test results, it was indicated that the specimen retrofitted with BRBs showed much better seismic performance than the control specimen without BRBs, and the BRBs could effectively improve the seismic performance of the reinforced concrete frame. For the specimen retrofitted with BRBs, the BRBs firstly yielded before the beam-ends and the column-ends, and an expected yielding process or yielding mechanism as well as good seismic performance was obtained. For the specimens without BRBs, though the beam-ends yielded prior to the column-ends, the seismic performance was much poor than that of the specimen with BRBs.

• Structural Engineering and Mechanics
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• 제60권6호
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• pp.1063-1077
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• 2016

Components manufactured from composite materials are frequently subjected to superimposed mechanical and thermal loadings during their operating service. Both types of loadings may cause fracture and failure of composite structures. When composite cross-ply laminates of type [$0_m/90_n]_s$ are subjected to uni-axial tensile loading, different types of damage are set-up and developed such as matrix cracking: transverse and longitudinal cracks, delamination between disoriented layers and broken fibers. The development of these modes of damage can be detrimental for the stiffness of the laminates. From the experimental point of view, transverse cracking is known as the first mode of damage. In this regard, the objective of the present paper is to investigate the effect of transverse cracking in cross-ply laminate under thermo-mechanical degradation. A Finite Element (FE) simulation of damage evolution in composite crossply laminates of type [$0_m/90_n]_s$ subjected to uni-axial tensile loading is carried out. The effect of transverse cracking on the cross-ply laminate strength under thermo-mechanical degradation is investigated numerically. The results obtained by prediction of the numerical model developed in this investigation demonstrate the influence of the transverse cracking on the bearing capacity and resistance to damage as well as its effects on the variation of the mechanical properties such as Young's modulus, Poisson's ratio and coefficient of thermal expansion. The results obtained are in good agreement with those predicted by the Shear-lag analytical model as well as with the obtained experimental results available in the literature.

• Steel and Composite Structures
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• 제52권2호
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• pp.121-134
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• 2024

To investigate the compressive behavior of partially encased recycled aggregate concrete (PERAC) stub columns after exposed to elevated temperatures, 22 specimens were tested. The maximum temperature suffered, the replacement ratio of recycled coarse aggregate (RCA), the endurance time and the spacing between links were considered as the main parameters. It was found that the failure mode of post-heated PERAC columns generally matched that of traditional partially encased composite (PEC) columns, but the flange of specimens appeared premature buckling after undergoing the temperature of 400℃ and above. Additionally, the ultimate strength and ductility of the specimens deteriorated with the elevated temperatures and extended heating time. When 400℃< T ≤ 600℃, the strength reduction range is the largest, about 11% ~ 17%. The higher the replacement ratio of RCA, the lower the ultimate strength of specimens. At the temperature of 600℃, the ultimate strength of specimens with the RCA replacement ratio of 50% and 100% is 0.94 and 0.91 times than that of specimens without RCA, respectively. But the specimen with 50% replacement ratio of RCA showed the best ductility performance. And the bearing capacity and ductility of PERAC stub columns were changed for the better due to the application of links. When the RCA replacement ratio is 100%, the ultimate strength of specimens with the link spacing of 100 mm and 50 mm increased 14% and 25% than that of the specimen without links, respectively. Based on the results above, a formula for calculating the ultimate strength of PERAC stub columns after exposure to high temperatures was proposed.

• Tribology and Lubricants
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• 제36권2호
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• pp.105-115
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• 2020

This paper presents a numerical study on the rotordynamic analysis of a dual-spool turbofan engine in the context of blade defect events. The blades of an axial-type aeroengine are typically well aligned during the compressor and turbine stages. However, they are sometimes exposed to damage, partially or entirely, for several operational reasons, such as cracks due to foreign objects, burns from the combustion gas, and corrosion due to oxygen in the air. Herein, we designed a dual-spool rotor using the commercial 3D modeling software CATIA to simulate blade defects in the turbofan engine. We utilized the rotordynamic parameters to create two finite element Euler-Bernoulli beam models connected by means of an inter-rotor bearing. We then applied the unbalanced forces induced by the mass eccentricities of the blades to the following selected scenarios: 1) fully balanced, 2) crack in the low-pressure compressor (LPC) and high pressure compressor (HPC), 3) burn on the high-pressure turbine (HPT) and low pressure compressor, 4) corrosion of the LPC, and 5) corrosion of the HPC. Additionally, we obtained the transient and steady-state responses of the overall rotor nodes using the Runge-Kutta numerical integration method, and employed model reduction techniques such as component mode synthesis to enhance the computational efficiency of the process. The simulation results indicate that the high-vibration status of the rotor commences beyond 10,000 rpm, which is identified as the first critical speed of the lower speed rotor. Moreover, we monitored the unbalanced stages near the inter-rotor bearing, which prominently influences the overall rotordynamic status, and the corrosion of the HPC to prevent further instability. The high-speed range operation (>13,000 rpm) coupled with HPC/HPT blade defects possibly presents a rotor-case contact problem that can lead to catastrophic failure.

• 한국구조물진단유지관리공학회 논문집
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• 제27권1호
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• pp.78-85
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• 2023

이 연구는 하이브리드 섬유시트를 이용하여 보강된 철근콘크리트 기둥의 구조성능평가에 관한 연구이다. 내진보강 공법은 보강이 필요한 노후 콘크리트 구조물에 아라미드섬유와 PET섬유를 일축으로 배열하여 직조한 하이브리드 섬유시트를 에폭시로 함침하고, 이를 구조물에 부착시켜 보강 구조물의 내하력을 증진시키는데 그 목적이 있다. 특히, 강재보다 가벼운 섬유를 사용함으로써 얻어지는 재료의 경량화뿐만 아니라, 사용된 섬유 중 저강도 고인성의 섬유요소가 고강도 저인성 섬유요소의 취성적 파괴를 지연시켜 기존의 섬유보강 공법과 비교해 안전성 측면에서 우수하다. 연구는 구조실험과 그 결과에 대한 구조성능평가로 진행되었다. 총 4개의 실험체는 하이브리드 보강방법 및 파괴모드를 주요변수로 계획하였으며, 실험체 크기 및 가력조건 등은 기존연구에서 수행한 실험결과와 비교가 가능하도록 계획하였다. 실험체의 구조성능은 에너지소산능력, 연성평가등을 사용하여 평가하였다. 다음과 같은 분석을 통하여 하이브리드 섬유시트의 보강하였을 때 우수한 성능 결과를 보일 수 있다는 결론은 얻었다.