• Title/Summary/Keyword: 강성 효과

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차량의 제동이 교량에 미치는 영향

  • 곽종원
    • Computational Structural Engineering
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    • v.10 no.4
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    • pp.30-33
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    • 1997
  • 차량의 제동에 의한 기존의 연구는 차량의 bounce와 pitch에 의한 차량의 거동특성에 따른 고려만이 이루어져 왔으며 교량의 수직방향 offset에 의한 고려는 이루어지지 않았다. 여기서 교량의 offset이란 교량의 주형과 상판 그리고 교좌부의 중심간에 수직방향 높이의 차이를 말하며, 차량의 제동이 발생할 때 이러한 offset에 의한 추가적인 휨거동이 발생하므로 이러한 offset을 고려하여야 한다. 아울러 고속철도와 같은 중차량의 경우에는 교각의 상대적인 강성에 의한 효과도 고려되어야 할 것이다.

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Finite Element Analysis for Transmission Tower Behavior Characteristic by Connection Beam Stiffness (수치해석을 이용한 송전철탑 연결형 기초의 연결보 강성에 따른 거동 특성)

  • Choi, YoungHo;Kyung, DooHyun;Lee, JunHwan
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.33 no.1
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    • pp.219-227
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    • 2013
  • This study analyzed the effect of performance connected-type foundations of behavior and the connected beams according to the characteristics into soft clay transmission tower foundation. For this purpose, the finite element analysis model was built and connected to the transmission tower foundation mat and the contact area of the connection beam by the percentage change in the behavior and resistance characteristics were analyzed and finite element verification of the validity of the analytical model was conducted using connected-type transmission tower results of the model experiments constructed, and effective connected-type transmission tower basis of the behavior of connected beams were selected by analyzing the effect due to the increase of the stiffness. In addition, weak analysis by connected beam self-bending moment distribution was conducted.

Seismic Performance of Precast Beam-Column Joints with Thru-Connectors (관통형 연결재로 연결된 PC 보-기둥 맞댐 접합의 내진성능에 관한 실험적 연구)

  • Park, Soon-Kyu;Kim, Min-Hee
    • Journal of the Korea Concrete Institute
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    • v.22 no.4
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    • pp.441-450
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    • 2010
  • This is a preliminary study on the development of precast beam-column joints for dry construction methodology. Precast beam column joints with thru-connectors (BCJ_TC) using high strength bars or PS strands were developed and their seismic performance including strength degradation, stiffness degradation and energy dissipation capacity was experimentally evaluated. Test results showed that compressive failures at the end blocks of PC beam members occurred dominantly while PC columns including panel zones were free from any damage. However, the connections confined with CFRP at the end block showed much improved seismic performance than that of the unconfined connections. Connections with neoprene pad fillers between beam and column interfaces were better than the other connections in all the seismic performances except initial stiffness. To improve the seismic performances of BCJ_TC, compressive strength of the concrete at the end block need to be increased to compensate for the additional compressive stresses due to unbonded connectors and deformation of connectors should be controlled respectively.

Material Nonlinear Analysis of the RC Shells Considering Tension Stiffening Effects (인장강성 효과를 고려한 RC 쉘의 재료비선형 해석)

  • Jin, Chi Sub;Eom, Jang Sub
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.13 no.5
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    • pp.99-107
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    • 1993
  • In this study, material nonlinear finite element program is developed to analyze reinforced concrete shell of arbitrary geometry considering tension stiffening effects. This study is capable of tracing the load-deformation response and crack propagation, as well as determining the internal concrete and steel stresses through the elastic, inelastic and ultimate ranges in one continuous computer analysis. The cracked shear retention factor is introduced to estimate the effective shear modulus including aggregate interlock and dowel action. The concrete is assumed to be brittle in tension and elasto-plastic in compression. The Drucker-Prager yield criterion and the associated flow rule are adopted to govern the plastic behavior of the concrete. The reinforcing bars are considered as a steel layer of equivalent thickness. A layered isoparametric flat finite element considering the coupling effect between the in-plane and the bending action was developed. Mindlin plate theory taking account of transverse shear deformation was used. An incremental tangential stiffness method is used to obtain a numerical solution. Numerical examples about reinforced concrete shell are presented. Validity of this method is studied by comparing with the experimential results of Hedgren and the numerical analysis of Lin.

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Evaluation of Aerodynamic Characteristics of NREL Phase VI Rotor System Using 2-Way Fluid-Structure Coupled Analysis Based on Equivalent Stiffness Model (등가강성모델 기반의 양방향 유체구조 연성해석을 적용한 NREL Phase VI 풍력 로터 시스템의 공력특성 평가)

  • Cha, Jin-Hyun;Song, Woo-Jin;Kang, Beom-Soo;Kim, Jeong
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.36 no.7
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    • pp.731-738
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    • 2012
  • In this study, the evaluation of the aerodynamic characteristics of the NREL Phase VI Rotor System has been performed, for the 7 m/s upwind case using commercial FEA and CFD tools which are ANSYS Mechanical 12.1 and CFX 12.1. The initial operating conditions of the rotor blade include a $3^{\circ}$ tip pitch angle. A numerical simulation was carried out on only the rotor parts, excluding the tower structure based on the equivalent stiffness model, to consider the aeroelastic effect for the numerical simulation using the loosely coupled 2-way fluid-structure interaction method. The blade root bending moment was monitored in real time to obtain reasonable results. To verify the analysis results, the numerical simulation results were compared with the measurements in the form of the root bending moment and the pressure distributions of the NREL/NASA Ames wind tunnel test.

Parametric Study on the Finite Element Idealization Method for Multi-Spar WIng (다중스파 날개의 유한요소 이상화 방법에 관한 인자연구)

  • Kweon, Jin-Hwe;Kang, Gyong-guk;Park, Chan-Woo;Kim, Seung-Ho
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.30 no.6
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    • pp.107-115
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    • 2002
  • A parametric study has been conducted to evaluate the effects of finite element modeling methods on the internal loads, sizing and the weight of the multi-spar aircraft wing structures. The wing is idealized into total 18finite element models and subjected to 4typical external load conditions. An automatic sizing algorithm based on MSC/NASTRAN and MSC/PATRAN is developed. The results show that the critical part affection the internal loads and weight of the structure is wing skin. Effect of modeling of the spar and rib on the structural behavior is not manifest. On the contrast to the general expectation, the models using the bending-resistant elements show the heavier weight than ones by the elements without bending stiffness. From this results, designers of multi-spar wing are recommended to construct the finite element model considering the bending stiffness, or to check the characteristics of the structure before modeling.