• 제목/요약/키워드: nonlinear response analysis

검색결과 1,456건 처리시간 0.023초

Analysis of extended end plate connection equipped with SMA bolts using component method

  • Toghroli, Ali;Nasirianfar, Mohammad Sadegh;Shariati, Ali;Khorami, Majid;Paknahad, Masoud;Ahmadi, Masoud;Gharehaghaj, Behnam;Zandi, Yousef
    • Steel and Composite Structures
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    • 제36권2호
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    • pp.213-228
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    • 2020
  • Shape Memory Alloys (SMAs) are new materials used in various fields of science and engineering, one of which is civil engineering. Owing to their distinguished capabilities such as super elasticity, energy dissipation, and tolerating cyclic deformations, these materials have been of interest to engineers. On the other hand, the connections of a steel structure are of paramount importance because of their vulnerabilities during an earthquake. Therefore, it is indispensable to find approaches to augment the efficiency and safety of the connection. This research investigates the behavior of steel connections with extended end plates equipped hybridly with 8 rows of high strength bolts as well as Nitinol superelastic SMA bolts. The connections are studied using component method in dual form. In this method, the components affecting the connections behavior, such as beam flange, beam web, column web, extended end plate, and bolts are considered as parallel and series springs according to the Euro-Code3. Then, the nonlinear force- displacement response of the connection is presented in the form of moment-rotation curve. The results obtained from this survey demonstrate that the connection has ductility, in addition to its high strength, due to high ductility of SMA bolts.

Design and Analysis of High-Speed Unmanned Aerial Vehicle Ground Directional Rectifying Control System

  • Yin, Qiaozhi;Nie, Hong;Wei, Xiaohui;Xu, Kui
    • International Journal of Aeronautical and Space Sciences
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    • 제18권4호
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    • pp.623-640
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    • 2017
  • The full nonlinear equations of an unmanned aerial vehicle ground taxiing mathematical dynamic model are built based on a type of unmanned aerial vehicle data in LMS Virtual.Lab Motion. The flexible landing gear model is considered to make the aircraft ground motion more accurate. The electric braking control system is established in MATLAB/Simulink and the experiment of it verifies that the electric braking model with the pressure sensor is fitted well with the actual braking mechanism and it ensures the braking response speediness. The direction rectification control law combining the differential brake and the rudder with 30% anti-skid brake is built to improve the directional stability. Two other rectifying control laws are demonstrated to compare with the designed control law to verify that the designed control is of high directional stability and high braking efficiency. The lateral displacement increases by 445.45% with poor rectification performance under the only rudder rectifying control relative to the designed control law. The braking distance rises by 36m and the braking frequency increases by 85.71% under the control law without anti-skid brake. Different landing conditions are simulated to verify the good robustness of the designed rectifying control.

Influence of bi-directional seismic pounding on the inelastic demand distribution of three adjacent multi-storey R/C buildings

  • Skrekas, Paschalis;Sextos, Anastasios;Giaralis, Agathoklis
    • Earthquakes and Structures
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    • 제6권1호
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    • pp.71-87
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    • 2014
  • Interaction between closely-spaced buildings subject to earthquake induced strong ground motions, termed in the literature as "seismic pounding", occurs commonly during major seismic events in contemporary congested urban environments. Seismic pounding is not taken into account by current codes of practice and is rarely considered in practice at the design stage of new buildings constructed "in contact" with existing ones. Thus far, limited research work has been devoted to quantify the influence of slab-to-slab pounding on the inelastic seismic demands at critical locations of structural members in adjacent structures that are not aligned in series. In this respect, this paper considers a typical case study of a "new" reinforced concrete (R/C) EC8-compliant, torsionally sensitive, 7-story corner building constructed within a block, in bi-lateral contact with two existing R/C 5-story structures with same height floors. A non-linear local plasticity numerical model is developed and a series of non-linear time-history analyses is undertaken considering the corner building "in isolation" from the existing ones (no-pounding case), and in combination with the existing ones (pounding case). Numerical results are reported in terms of averages of ratios of peak inelastic rotation demands at all structural elements (beams, columns, shear walls) at each storey. It is shown that seismic pounding reduces on average the inelastic demands of the structural members at the lower floors of the 7-story building. However, the discrepancy in structural response of the entire block due to torsion-induced, bi-directionally seismic pounding is substantial as a result of the complex nonlinear dynamics of the coupled building block system.

트랙터 캐빈의 진동저감을 위한 방진고무의 형상최적설계 (Shape Optimal Design of Anti-Vibration Rubber Assembly to Reduce the Vibration of a Tractor Cabin)

  • 최효준;이상훈
    • 한국산학기술학회논문지
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    • 제19권4호
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    • pp.657-663
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    • 2018
  • 본 연구에서는 농업용 트랙터에 조립식으로 결합되는 캐빈에 사용되는 방진고무의 진동절연성능을 향상시키기 위하여 형상최적설계를 수행하였다. 초탄성거동을 보이는 고무의 물성을 평가하기 위하여 일축 및 이축 인장시험을 수행하였고 이를 이용하여 유한요소해석에 입력 가능한 재료 모델을 도출하였다. 실제 트랙터의 운전 상태에서 진동을 측정하여 방진고무로 전달되는 입력 가진 및 이로 인한 캐빈 프레임의 응답을 정량화하였다. 비선형 거동을 보이는 방진고무의 특성을 반영하기 위해 정해석을 이용하여 방진고무의 하중-변위 곡선을 도출하였다. 이로부터 특정 하중 혹은 변위가 가해진 상태에서 방진고무의 강성을 계산할 수 있었으며 이를 캐빈의 조화가진해석에 사용하였다. 해석결과와 시험 결과의 비교를 통하여 해석모델 및 기법의 타당성을 검증하였다. 방진고무의 형상설계를 위하여 다구찌의 인자설계법이 사용되었으며 이를 통하여 강성이 최소화된 방진고무의 형상을 찾을 수 있었다. 방진고무의 최적 형상을 고려하여 조화가진해석을 수행한 결과 초기설계 대비 35 % 이상 개선된 진동저감효과를 확인할 수 있었다.

등분포하중에 종속된 폼내장 콘크리트 샌드위치패널의 유한변위거동 (Large Displacement Behaviors of Foam-Insulated Concrete Sandwich Panels Subjected to Uniform Pressure)

  • 강준석;원덕희;강영종
    • 복합신소재구조학회 논문집
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    • 제2권4호
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    • pp.35-43
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    • 2011
  • 본 연구는 등분포 하중에 종속된 폼내장 콘크리트 샌드위치 패널 (foam insulated concrete sandwich panel)의 구조거동특성을 파악하였다. 유한요소모델이 콘크리트, 폼 그리고 철근의 비선형거동과 연결부재 (connector)의 상세 전단저항거동을 모사하기위해 사용되었다. 개발된 모델은 미주리대학 (University of Missouri)에서 수행된 정적실험자료를 사용하여 검증되었다. 합성 및 비합성 거동이 샌드위치패널의 구조거동에 미치는 영향을 정확히 모사하기 위해 전단연결재의 저항력을 모델에 정확히 반영하는 것이 중요하다. 본 연구에서 개발된 모델은 구조물의 극한강도 및 좌굴이후의 거동까지 모사하였고 미국콘크리트 학회 (ACI)의 설계예제와 비교하였다. 본연구의 결과는 정적 및 동적하중에 종속된 폼내장 콘크리트 샌드위치 패널의 해석및 설계에 유용한 정보를 제공할 것이다.

비정형 셀프센터링 가새골조의 비탄성 지진응답 (Inelastic Seismic Response of Asymmetric-Plan Self-Centering Energy Dissipative Braced Frames)

  • 김진구;;최현훈
    • 한국지진공학회논문집
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    • 제12권4호
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    • pp.35-44
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    • 2008
  • 최근 새로운 지진하중 저항시스템으로 셀프센터링(SCED) 가새 시스템이 개발되었다. 진보된 가새 시스템인 비좌굴 가새(BRB) 시스템과는 달리 큰 지진이 발생한 후 구조물의 잔류 변형을 줄이거나 없앨 수 있는 셀프센터링 능력은 SCED 가새 시스템의 장점이다. 본 논문에서는 SCED 가새와 BRB 가새 시스템의 거동에 비틀림의 영향을 조사하기 위하여 세 가지 다른 편심을 가진 3차원 구조물의 응답을 비선형 동적해석을 수행하여 비교하였다. 해석결과에 따르면 층간변위의 높이방향의 변화는 비정형성에 관계없이 SCED 가새골조의 응답이 BRB 가새골조보다 일정하였으며, 잔류 층간변위와 잔류 회전 응답은 비정형성이 증가함에 따라 감소하였다. 중층 구조물에서 SCED 가새골조의 변형집중계수(DCF)는 BRB 가새골조보다 작은 것으로 나타났다. 이것은 SCED 가새골조가 건물 높이에 따라 보다 일정하게 변형함을 의미한다. DCF의 크기에 대한 비틀림 비정형의 효과는 작았다.

Contact interface fiber section element: shallow foundation modeling

  • Limkatanyu, Suchart;Kwon, Minho;Prachasaree, Woraphot;Chaiviriyawong, Passagorn
    • Geomechanics and Engineering
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    • 제4권3호
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    • pp.173-190
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    • 2012
  • With recent growing interests in the Performance-Based Seismic Design and Assessment Methodology, more realistic modeling of a structural system is deemed essential in analyzing, designing, and evaluating both newly constructed and existing buildings under seismic events. Consequently, a shallow foundation element becomes an essential constituent in the implementation of this seismic design and assessment methodology. In this paper, a contact interface fiber section element is presented for use in modeling soil-shallow foundation systems. The assumption of a rigid footing on a Winkler-based soil rests simply on the Euler-Bernoulli's hypothesis on sectional kinematics. Fiber section discretization is employed to represent the contact interface sectional response. The hyperbolic function provides an adequate means of representing the stress-deformation behavior of each soil fiber. The element is simple but efficient in representing salient features of the soil-shallow foundation system (sliding, settling, and rocking). Two experimental results from centrifuge-scale and full-scale cyclic loading tests on shallow foundations are used to illustrate the model characteristics and verify the accuracy of the model. Based on this comprehensive model validation, it is observed that the model performs quite satisfactorily. It resembles reasonably well the experimental results in terms of moment, shear, settlement, and rotation demands. The hysteretic behavior of moment-rotation responses and the rotation-settlement feature are also captured well by the model.

Experimental research on the propagation of plastic hinge length for multi-scale reinforced concrete columns under cyclic loading

  • Tang, Zhenyun;Ma, Hua;Guo, Jun;Xie, Yongping;Li, Zhenbao
    • Earthquakes and Structures
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    • 제11권5호
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    • pp.823-840
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    • 2016
  • The plastic hinge lengths of beams and columns are a critical demand parameter in the nonlinear analysis of structures using the finite element method. The numerical model of a plastic hinge plays an important role in evaluating the response and damage of a structure to earthquakes or other loads causing the formation of plastic hinges. Previous research demonstrates that the plastic hinge length of reinforced concrete (RC) columns is closely related to section size, reinforcement ratio, reinforcement strength, concrete strength, axial compression ratio, and so on. However, because of the limitations of testing facilities, there is a lack of experimental data on columns with large section sizes and high axial compression ratios. In this work, we conducted a series of quasi-static tests for columns with large section sizes (up to 700 mm) and high axial compression ratios (up to 0.6) to explore the propagation of plastic hinge length during the whole loading process. The experimental results show that besides these parameters mentioned in previous work, the plastic hinge of RC columns is also affected by loading amplitude and size effect. Therefore, an approach toward considering the effect of these two parameters is discussed in this work.

Cyclic response and design procedure of a weak-axis cover-plate moment connection

  • Lu, Linfeng;Xu, Yinglu;Zheng, Huixiao;Lim, James B.P.
    • Steel and Composite Structures
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    • 제26권3호
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    • pp.329-345
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    • 2018
  • This paper systematically investigated the mechanical performance of the weak-axis cover-plate connection, including a beam end monotonic loading test and a column top cyclic loading test, and a series of parametric studies for exterior and interior joints under cyclic loading using a nonlinear finite element analysis program ABAQUS, focusing on the influences of the shape of top cover-plate, the length and thickness of the cover-plate, the thickness of the skin plate, and the steel material grade. Results showed that the strains at both edges of the beam flange were greater than the middle's, thus it is necessary to take some technical methods to ensure the construction quality of the beam flange groove weld. The plastic rotation of the exterior joint can satisfy the requirement of FEMA-267 (1995) of 0.03 rad, while only one side connection of interior joint satisfied ANSI/AISC 341-10 under the column top cyclic loading. Changing the shape or the thickness or the length of the cover-plate did not significantly affect the mechanical behaviors of frame joints no matter in exterior joints or interior joints. The length and thickness of the cover-plate recommended by FEMA 267 (1995) is also suitable to the weak-axis cover-plate joint. The minimum skin plate thickness and a design procedure for the weak-axis cover-plate connections were proposed finally.

곡률을 가진 적층복합재 구조에서의 저속충격손상 평가 (Damage Assessment of Curved Composite Laminate Structures Subjected to Low-Velocity Impact)

  • 전정규;권오양;이우식
    • Composites Research
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    • 제14권2호
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    • pp.22-32
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    • 2001
  • 유한한 곡률을 가진 적층복합재 구조의 저속충격손상을 평가하기 위하여 곡률반경이 각각 50, 150, 300, 500 mm인 쉘 형태의 시편을 CFRP로 제작하여 충격실험을 행하고, 충격거동과 충격손상을 평판의 경우와 비교하여 고찰하였다. 실험결과는 비선형 유한요소해석의 결과와 비교하였다. 충격손상의 평가를 위해 충격거동을 측정한 결과 강성과 곡률반경이 쉘의 동적 충격거동에 큰 영향을 미치는 것을 확인하였으며, 충격거동과 충격손상은 밀접한 상호관계가 있으므로 구조의 곡률반경을 독립변수로 선정하여 충격손상을 평가하였다. 곡률반경이 감소하면서 복합재 쉘에는 동일한 충격조건에서 더 큰 최대 접촉력이 발생하였고, 가장 곡률이 심한 곡률반경 50 mm의 쉘에서는 평판의 약 1.5배에 이르는 최대 접촉력을 나타내었다. 따라서 동일한 충격조건 하에서 곡률반경 50 mm의 쉘에서는 평판의 경우보다 약 2.7때정도 더 큰 층간분리가 내부에 발생하였으며, 층간분리의 분포 또한 평판의 경우와는 달리 충격면에 가까운 계면에도 광범위하게 발생하는 경향이 곡륜반경이 감소할수록 더욱 현저하였다. 이는 곡률을 가진 구조가 평판 구조보다 손상저항성이 더 작은 것을 의미하므로 복합재료 설계 시 구조의 기하학적 형상을 반드시 고려하여야 한다.

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