• 제목/요약/키워드: the structural layer coefficient

검색결과 96건 처리시간 0.027초

A comprehensively overall track-bridge interaction study on multi-span simply supported beam bridges with longitudinal continuous ballastless slab track

  • Su, Miao;Yang, Yiyun;Pan, Rensheng
    • Structural Engineering and Mechanics
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    • 제78권2호
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    • pp.163-174
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    • 2021
  • Track-bridge interaction has become an essential part in the design of bridges and rails in terms of modern railways. As a unique ballastless slab track, the longitudinal continuous slab track (LCST) or referred to as the China railway track system Type-II (CRTS II) slab track, demonstrates a complex force mechanism. Therefore, a comprehensive track-bridge interaction study between multi-span simply supported beam bridges and the LCST is presented in this work. In specific, we have developed an integrated finite element model to investigate the overall interaction effects of the LCST-bridge system subjected to the actions of temperature changes, traffic loads, and braking forces. In that place, the deformation patterns of the track and bridge, and the distributions of longitudinal forces and the interfacial shear stress are studied. Our results show that the additional rail stress has been reduced under various loads and the rail's deformation has become much smoother after the transition of the two continuous structural layers of the LCST. However, the influence of the temperature difference of bridges is significant and cannot be ignored as this action can bend the bridge like the traffic load. The uniform temperature change causes the tensile stress of the concrete track structure and further induce cracks in them. Additionally, the influences of the friction coefficient of the sliding layer and the interfacial bond characteristics on the LCST's performance are discussed. The systematic study presented in this work may have some potential impacts on the understanding of the overall mechanical behavior of the LCST-bridge system.

Structural and Optical Properties of Copper Indium Gallium Selenide Thin Films Prepared by RF Magnetron Sputtering

  • Kong, Seon-Mi;Fan, Rong;Kim, Dong-Chan;Chung, Chee-Won
    • 한국진공학회:학술대회논문집
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    • 한국진공학회 2011년도 제40회 동계학술대회 초록집
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    • pp.158-158
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    • 2011
  • $Cu(In_xGa_{1-x})Se_2$ (CIGS) thin film solar cell is one of the most promising solar cells in photovoltaic devices. CIGS has a direct band gap which varied from 1.0 to 1.26 eV, depending on the Ga to In ratio. Also, CIGS has been studying for an absorber in thin film solar cells due to their highest absorption coefficient which is $1{\times}10^5cm^{-1}$ and good stability for deposition process at high temperature of $450{\sim}590^{\circ}C$. Currently, the highest efficiency of CIGS thin film solar cell is approximately 20.3%, which is closely approaching to the efficiency of poly-silicon solar cell. The deposition technique is one of the most important points in preparing CIGS thin film solar cells. Among the various deposition techniques, the sputtering is known to be very effective and feasible process for mass production. In this study, CIGS thin films have been prepared by rf magnetron sputtering method using a single target. The optical and structural properties of CIGS films are generally dependent on deposition parameters. Therefore, we will explore the influence of deposition power on the properties of CIGS films and the films will be deposited by rf magnetron sputtering using CIGS single target on Mo coated soda lime glass at $500^{\circ}C$. The thickness of CIGS films will be measured by Tencor-P1 profiler. The optical properties will be measured by UV-visible spectroscopy. The crystal structure will be analyzed using X-ray diffraction (XRD). Finally the optimal deposition conditions for CIGS thin films will be developed.

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구조보강용 FRP 복합체의 역학적 특성치 분석을 위한 인장시험방법 평가 연구 (Appraisal Study on Tensile Test Method of Mechanical Properties of FRP Composite Used in Strengthening RC Members)

  • 유영찬;최기선;강인석;김긍환
    • 한국구조물진단유지관리공학회 논문집
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    • 제12권1호
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    • pp.73-80
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    • 2008
  • 본 논문에서는 RC 구조물의 보수 보강 공사에 적용되는 FRP 복합체의 역학적 특성치를 평가하기 위하여 각국에서 제안된 시험규격을 비교 분석하고, 시험편 형상 및 시험방법의 차이가 재료성능에 미치는 영향에 대한 실험적 검증을 통하여 표준화된 시험방법 및 평가기준을 도출하고자 하였다. 주 실험변수는 FRP 복합체의 종류, 시험편의 폭, 보강매수 및 가력속도로 설정하였다. 본 시험결과에 의하면, 최대 인장강도와 최소변동계수를 나타내는 인장 시험편의 폭은 FRP의 종류/직조방법에 따라 다르게 나타났으며, 특히 적층형으로 시공되는 FRP 복합체는 보강매수에 따른 인장강도의 저하현상이 관측되므로, 이를 적절히 고려할 수 있는 평가기준의 설정이 필요할 것으로 판단된다.

알루미늄 판상에 글라스 세라믹 후막이 코팅된 절연금속기판의 제조 및 절연특성 (Fabrication and Electrical Insulation Property of Thick Film Glass Ceramic Layers on Aluminum Plate for Insulated Metal Substrate)

  • 이성환;김효태
    • 마이크로전자및패키징학회지
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    • 제24권4호
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    • pp.39-46
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    • 2017
  • 본 연구는 평판형 히터용 금속방열판상의 세라믹 절연층 제조, 즉 절연성 금속기판에 관한 것이다. 반도체나 디스플레이의 열처리 공정 등에 사용되는 평판형 히터를 제조함에 있어서, 온도 균일도를 높이기 위해 금속 방열판으로서 열전도율이 높고, 비교적 가벼우며, 가공성 좋은 알루미늄 합금 기판이 선호된다. 이 알루미늄 기판에 발열 회로 패턴을 형성하기 위해서는 금속 기판에 절연층으로서 고온 안정성이 우수한 세라믹 유전체막을 코팅하여야 한다. 금속 기판상에 세라믹 절연층을 형성함에 있어서 가장 빈번히 발생하는 첫 번째 문제는 금속과 세라믹의 이종재료 간의 큰 열팽창계수 차이와 약한 결합력에 의한 층간박리 및 균열발생이다. 두 번째 문제는 절연층의 소재 및 구조적 결함에 따른 절연파괴이다. 본 연구에서는 이러한 문제점 해소를 위해 금속소재 기판과 세라믹 절연층 사이에 완충층을 도입하여 이들 간의 기계적 매칭과 접합력 개선을 도모하였고, 다중코팅 방법을 적용하여 절연막의 품질과 내전압 특성을 개선하고자 하였다.

모발의 마찰계수를 통한 모발 손상 인식 연구 (A Study for Perception of Hair Damage Using Friction Coefficient of Human Hair)

  • 임병택;서홍안;송상훈;손성길;강내규
    • 대한화장품학회지
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    • 제46권3호
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    • pp.295-305
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    • 2020
  • 염색과 같이 산화제를 이용한 미용은 모발의 큐티클 구조를 바꾸거나 단백질 변성 및 지질의 소실을 야기하여 모발을 손상시킨다. 본 연구에서는 모발 손상 변화를 기기 평가를 통해 마찰계수를 측정하고 이것이 소비자들의 손상 인지와 상관성이 있는지 알아보고, 더 나아가 손상 원인을 수분 변화에서 찾아 분석 하였다. 염색, 펌, 탈색 과정을 모발에 반복할 때 마찰계수를 측정한 결과 염색의 경우는 3 회 처리에서 마찰계수 0.60을 기록했는데, 일반인들을 대상으로 동일 모발에 대한 촉감에 의한 손상 인지 조사에서 응답자의 58%가 이 모발에서 처음으로 손상을 인지한다고 답하였다. 탈색의 경우 3 회 처리에서 마찰계수가 0.84 로 크게 변하였는데 응답자의 88%가 손상모로 인지하였다. 지질 소실을 통한 손상에 따른 인지를 알아보기 위하여 모발 표면의 18-methyleicosanoic acid (18-MEA)를 제거해가며 마찰계수를 인위적으로 높인 다양한 모발을 제작하였다. 이 경우 마찰계수가 0.60 인 모발부터 전체 응답자의 68%가 최초로 손상을 인식한다고 답하였다. 기기평가로 확인된 마찰계수와 이와 연관되는 손상 인지가 모발에서 가장 많은 양을 차지하는 수분으로부터 기여되는지 확인하기 위하여 손상모의 수분함량을 측정하였다. 염색 처리 횟수가 증가할수록 모발의 접촉각이 감소하며 모발이 친수성으로 변함을 확인하였는데, 실제로 염색 손상모가 건강한 모발보다 0.42% 더 많은 수분량을 가짐을 유의차 있게 확인하였다. 최종적으로는 손상 모발의 수분량 증가가 마찰계수와 비례하는 점착력 증가를 유도하며 마찰계수가 0.60 이상으로 증가할 때 손상 인지가 됨을 알아보았다.

통계분석 알고리즘 프로그램을 활용한 동시 인상 3D 콘크리트 프린팅의 성능 분석 (Performance Analysis of Simultaneous Liftable 3D Concrete Printing Based on Statistical Analysis Algorithm)

  • 김윤철;김성조;김봉식;지용수;한동석
    • 한국전산구조공학회논문집
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    • 제36권6호
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    • pp.407-414
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    • 2023
  • 본 논문에서는 다양한 분야에 적용할 수 있는 자동화 동시 인상 시스템을 3D 콘크리트 프린팅에 적용하여 동시 인상이 가능한 3D 콘크리트 프린팅 시스템으로 개발하였다. 개발된 시스템은 3D 콘크리트 프린팅 작업 중 측정되는 인상량을 피어슨 상관계수를 통해 분석하고, 유압시스템을 사분위수 기법으로 실시간 모니터링하여 안전하고 정밀한 인상이 가능하다. 이를 활용하면 3D 콘크리트 프린팅 구조물의 출력 품질을 확보함과 동시에 3D 콘크리트 프린팅의 규모보다 큰 구조물을 출력할 수 있다. 시스템의 성능을 평가하기 위해 기존의 3D 콘크리트 프린팅과 동시 인상이 가능한 3D 콘크리트 프린팅을 각각 이용하여 시편을 출력하였다. 출력된 시편은 3D 스캐너를 활용하여 측정하였다. 스캔한 시편의 층별 직경과 시편의 교차각을 측정하였으며, 분석을 통해 동시 인상이 가능한 3D 콘크리트 프린팅의 성능을 검증하였다.

Calculating the collapse margin ratio of RC frames using soft computing models

  • Sadeghpour, Ali;Ozay, Giray
    • Structural Engineering and Mechanics
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    • 제83권3호
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    • pp.327-340
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    • 2022
  • The Collapse Margin Ratio (CMR) is a notable index used for seismic assessment of the structures. As proposed by FEMA P695, a set of analyses including the Nonlinear Static Analysis (NSA), Incremental Dynamic Analysis (IDA), together with Fragility Analysis, which are typically time-taking and computationally unaffordable, need to be conducted, so that the CMR could be obtained. To address this issue and to achieve a quick and efficient method to estimate the CMR, the Artificial Neural Network (ANN), Response Surface Method (RSM), and Adaptive Neuro-Fuzzy Inference System (ANFIS) will be introduced in the current research. Accordingly, using the NSA results, an attempt was made to find a fast and efficient approach to derive the CMR. To this end, 5016 IDA analyses based on FEMA P695 methodology on 114 various Reinforced Concrete (RC) frames with 1 to 12 stories have been carried out. In this respect, five parameters have been used as the independent and desired inputs of the systems. On the other hand, the CMR is regarded as the output of the systems. Accordingly, a double hidden layer neural network with Levenberg-Marquardt training and learning algorithm was taken into account. Moreover, in the RSM approach, the quadratic system incorporating 20 parameters was implemented. Correspondingly, the Analysis of Variance (ANOVA) has been employed to discuss the results taken from the developed model. Additionally, the essential parameters and interactions are extracted, and input parameters are sorted according to their importance. Moreover, the ANFIS using Takagi-Sugeno fuzzy system was employed. Finally, all methods were compared, and the effective parameters and associated relationships were extracted. In contrast to the other approaches, the ANFIS provided the best efficiency and high accuracy with the minimum desired errors. Comparatively, it was obtained that the ANN method is more effective than the RSM and has a higher regression coefficient and lower statistical errors.

Vortex induced vibration and flutter instability of two parallel cable-stayed bridges

  • Junruang, Jirawat;Boonyapinyo, Virote
    • Wind and Structures
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    • 제30권6호
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    • pp.633-648
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    • 2020
  • The objective of this work was to investigate the interference effects of two-parallel bridge decks on aerodynamic coefficients, vortex-induced vibration, flutter instability and flutter derivatives. The two bridges have significant difference in cross-sections, dynamic properties, and flutter speeds of each isolate bridge. The aerodynamic static tests and aeroelastic tests were performed in TU-AIT boundary layer wind tunnel in Thammasat University (Thailand) with sectional models in a 1:90 scale. Three configuration cases, including the new bridge stand-alone (case 1), the upstream new bridge and downstream existing bridge (case 2), and the downstream new bridge and the upstream existing bridge (case 3), were selected in this study. The covariance-driven stochastic subspace identification technique (SSI-COV) was applied to identify aerodynamic parameters (i.e., natural frequency, structural damping and state space matrix) of the decks. The results showed that, interference effects of two bridges decks on aerodynamic coefficients result in the slightly reduction of the drag coefficient of case 2 and 3 when compared with case 1. The two parallel configurations of the bridge result in vortex-induced vibrations (VIV) and significantly lower the flutter speed compared with the new bridge alone. The huge torsional motion from upstream new bridge (case 2) generated turbulent wakes flow and resulted in vertical aerodynamic damping H1* of existing bridge becomes zero at wind speed of 72.01 m/s. In this case, the downstream existing bridge was subjected to galloping oscillation induced by the turbulent wake of upstream new bridge. The new bridge also results in significant reduction of the flutter speed of existing bridge from the 128.29 m/s flutter speed of the isolated existing bridge to the 75.35 m/s flutter speed of downstream existing bridge.

핵연료 피복관용 다중층 SiC 복합체 튜브의 Hoop Stress 전산모사 연구 (FEA Study on Hoop Stress of Multilayered SiC Composite Tube for Nuclear Fuel Cladding)

  • 이현근;김대종;박지연;김원주
    • 한국세라믹학회지
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    • 제51권5호
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    • pp.435-441
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    • 2014
  • Silicon carbide-based ceramics and their composites have been studied for application to fusion and advanced fission energy systems. For fission reactors, $SiC_f$/SiC composites can be applied to core structural materials. Multilayered SiC composite fuel cladding, owing to its superior high temperature strength and low hydrogen generation under severe accident conditions, is a candidate for the replacement of zirconium alloy cladding. The SiC composite cladding has to retain its mechanical properties and original structure under the inner pressure caused by fission products; as such it can be applied as a cladding in fission reactor. A hoop strength test using an expandable polyurethane plug was designed in order to evaluate the mechanical properties of the fuel cladding. In this paper, a hoop strength test of the multilayered SiC composite tube for nuclear fuel cladding was simulated using FEA. The stress caused by the plug was distributed nonuniformly because of the friction coefficient difference between the inner surface of the tube and the plug. Hoop stress and shear stress at the tube was evaluated and the relationship between the concentrated stress at the inner layer of the tube and the fracture behavior of the tube was investigated.

3D Numerical investigation of a rounded corner square cylinder for supercritical flows

  • Vishwanath, Nivedan;Saravanakumar, Aditya K.;Dwivedi, Kush;Murthy, Kalluri R.C.;Gurugubelli, Pardha S.;Rajasekharan, Sabareesh G.
    • Wind and Structures
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    • 제35권1호
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    • pp.55-66
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    • 2022
  • Tall buildings are often subjected to steady and unsteady forces due to external wind flows. Measurement and mitigation of these forces becomes critical to structural design in engineering applications. Over the last few decades, many approaches such as modification of the external geometry of structures have been investigated to mitigate wind-induced load. One such proven geometric modification involved the rounding of sharp corners. In this work, we systematically analyze the impact of rounded corner radii on the reducing the flow-induced loading on a square cylinder. We perform 3-Dimensional (3D) simulations for high Reynolds number flows (Re=1 × 105) which are more likely to be encountered in practical applications. An Improved Delayed Detached Eddy Simulation (IDDES) method capable of capturing flow accurately at large Reynolds numbers is employed in this study. The IDDES formulation uses a k-ω Shear Stress Transport (SST) model for near-wall modelling that prevents mesh-induced separation of the boundary layer. The effects of these corner modifications are analyzed in terms of the resulting variations in the mean and fluctuating components of the aerodynamic forces compared to a square cylinder with no geometric changes. Plots of the angular distribution of the mean and fluctuating coefficient of pressure along the square cylinder's surface illustrate the effects of corner modifications on the different parts of the cylinder. The windward corner's separation angle was observed to decrease with an increase in radius, resulting in a narrower and longer recirculation region. Furthermore, with an increase in radius, a reduction in the fluctuating lift, mean drag, and fluctuating drag coefficients has been observed.