• 한국지반신소재학회논문집
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• 제18권2호
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• pp.11-21
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• 2019

본 연구에서는 말뚝의 인발저항에 대한 합리적 평가를 위하여, 다양한 지반 조건(상대밀도, 세립분 함유율)에서 말뚝의 인발거동 모사에 대한 유한요소해석의 적용성을 평가하였다. 즉, 기존의 실내모형실험 결과(You et al., 2018)를 대상으로 동일한 조건에서의 유한요소해석을 실시하였고, 유한요소해석에 이용된 해석모델의 신뢰성을 검증하였다. 또한 수치해석을 활용한 말뚝의 인발거동 모사에 대한 적정성을 평가하였다. 그 결과, 가상지반이 적용된 축대칭 해석을 이용하여 말뚝의 주면마찰력을 평가할 수 있는 것으로 확인되었다. 또한 다양한 지반 조건에 대하여 말뚝-지반 경계면의 전단저항 특성을 반영할 수 있는 축대칭 해석은 말뚝의 합리적인 인발거동 모사가 가능한 해석방법으로 활용이 가능한 것으로 분석되었다. 따라서 본 연구를 통하여 제안된 해석모델은 말뚝의 응력-변형 관계를 통한 인발거동을 적절하게 모사할 수 있는 것으로 판단되었다.

• 한국도로학회논문집
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• 제19권6호
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• pp.67-74
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• 2017

PURPOSES : In this study, a three-dimensional nonlinear finite element analysis (FEA) model for airport concrete pavement was developed using the commercial program ABAQUS. Users can select an analysis method and set the range of input parameters to reflect actual conditions such as environmental loading. METHODS : The geometrical shape of the FEA model was chosen by considering the concrete pavement located in the third-stage construction site of Incheon International Airport. Incompatible eight-node elements were used for the FEA model. Laboratory test results for the concrete specimens fabricated at the construction site were used as material properties of the concrete slab. The material properties of the cement-treated base suggested by the Federal Aviation Administration(FAA) manual were used as those of the lean concrete subbase. In addition, preceding studies and pavement evaluation reports of Incheon International Airport were referred for the material properties of asphalt base and subgrade. The kinetic friction coefficient between the concrete slab and asphalt base acquired from a preceding study was used for the friction coefficient between the layers. A nonlinear temperature gradient according to slab depth was used as an input parameter of environmental loading, and a quasistatic method was used to analyze traffic loading. The average load transfer efficiency obtained from an Heavy falling Weight Deflectomete(HWD) test was converted to a spring constant between adjacent slabs to be used as an input parameter. The reliability of the FEA model developed in this study was verified by comparing its analysis results to those of the FEAFAA model. RESULTS : A series of analyses were performed for environmental loading, traffic loading, and combined loading by using both the model developed in this study and the FEAFAA model under the same conditions. The stresses of the concrete slab obtained by both analysis models were almost the same. An HWD test was simulated and analyzed using the FEA model developed in this study. As a result, the actual deflections at the center, mid-edge, and corner of the slab caused by the HWD loading were similar to those obtained by the analysis. CONCLUSIONS : The FEA model developed in this study was judged to be utilized sufficiently in the prediction of behavior of airport concrete pavement.

• International Journal of Precision Engineering and Manufacturing
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• 제9권4호
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• pp.22-25
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• 2008

The dynamic response of the head arm assembly (HAA) of a hard disk drive to an impact load was obtained from a 3D non-linear finite element model using ANSYS/LS-DYNA and from experiments using a modified levitation mass method (LMM). In the finite element model, the impact load was created by modeling the mass as a rigid body and making it collide with the HAA. The velocity, displacement, acceleration, and inertial force of the mass were then obtained from the time history data of the finite element analysis. In the LMM, a mass that was levitated with an aerostatic linear bearing, and hence encountered negligible friction, was made to collide with the actuator arm, resulting in a dynamic bending test for the arm. During the collision, the Doppler frequency shift of the laser beam reflected from the mass was accurately measured with an optical interferometer. The velocity, displacement, acceleration, and inertial force of the mass were accurately calculated from the measured time-varying Doppler frequency shift. A good correlation between the experimental data and FEA results was observed. The FEA was also used to investigate the dynamic response of the HAA to impact by different masses.

• 한국구조물진단유지관리공학회 논문집
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• 제25권4호
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• pp.20-27
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• 2021

이 연구에서는 강봉 트러스 시스템으로 보강된 조적벽체의 내진거동을 합리적으로 평가하기 위하여 범용프로그램인 Abaqus를 이용한 비선형 유한요소해석 절차를 제시하였다. 조적벽체의 유한요소 모델은 콘크리트 손상 소성(concrete damaged plasticity, CDP)모델 및 벽돌-모르타르 계면 특성은 Yang et al.이 제시한 조적 프리즘의 압축 및 인장의 응력-변형률 모델과 전단마찰모델을 기반으로 메소-스케일법을 적용하였다. 유한요소 해석결과를 다양한 변수조건에서 실험결과와 비교한 결과, 강봉 트러스 시스템으로 보강된 조적벽체의 균열진전, 파괴 모드, 강체회전 내력 및 최대내력 그리고 횡하중-횡변위 관계에 대한 실험결과와 잘 일치하였다. 따라서 제시된 유한요소해석 절차는 조적벽체의 내진보강 설계에 합리적으로 이용될 수 있다고 판단된다.

• 한국지반신소재학회논문집
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• 제18권2호
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• pp.45-54
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• 2019

본 연구에서는 원지반의 상대밀도와 세립분 함유율의 조건에 따른 말뚝의 인발거동 특성 규명을 위하여, 유한요소해석을 수행하였다. 수치해석에서는 말뚝과 지반 경계에서의 전단거동을 원활히 모사하기 위해서 경계요소와 경계면 강도감소계수($R_{inter}$)를 부여하였으며, 그 결과를 기존의 실험적 연구결과(You et al., 2018)와 비교함으로써 본 수치해석 방법의 신뢰성을 검증하였고, 말뚝-지반 경계면에서의 변형 특성과 함께 경계요소에 대한 $R_{inter}$값의 결정방법을 제시하였다. 해석 결과, 본 연구에서 적용된 해석모델을 이용한 수치해석은 말뚝의 인발모형실험에 의한 말뚝과 지반의 경계면 특성을 적절하게 모사하였다. 또한 제시된 $R_{inter}$의 적용에 있어서, 반드시 지반의 상대밀도와 세립분 함유율 조건을 고려해야 할 필요가 있음을 확인하였다.

• 소성∙가공
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• 제19권8호
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• pp.494-501
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• 2010

The main objective of this study is to examine the sensitivity of calibration curves of FEA of ring compression test to frictional shear factor. Ring compression test has been investigated by measuring dimensional changes at different positions of ring specimen and they include the changes in internal diameter at the middle and top section of the specimen, outer diameter at the middle and top section, surface expansion at the top surface, respectively. Initial ring geometries employed in analysis maintain a fixed ratio of 6 : 3 : 2, i.e. outer diameter : inner diameter : thickness of the ring specimen, which is generally known as 'standard' specimen. A rigid plastic material for different work-hardening characteristics has been modeled for simulations using rigid-plastic finite element code. Analyses have been performed within a definite range of friction as well as over whole range of friction to show different sensitivities to the interfacial friction for different ranges of friction. The results of investigation in this study have been summarized in terms of a dimensionless gradient. It has been known from the results that the dimensional changes at different positions of ring specimen show different linearity and sensitivity to the frictional condition on the contact surface.

• Elastomers and Composites
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• 제50권4호
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• pp.251-257
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• 2015

The rubber seal is a part inserted into servo cylinder to keep the air pressure constant. In order for efficient movements of the servo cylinder, the frictional coefficient of the rubber seal needs to be minimized while the sealing is maintained. In this work the friction characteristics of rubber seal specimen are tested on metal plate at various conditions. The experimental conditions include roughness level, applied pressure, lubrication, and rubbing speed. The design of experiment approach is taken to assess the effect of each parameter. The nonlinear frictional response of the rubber is applied to the FEM model simulating the servo cylinder movement. The result demonstrates that precise optimization of the servo cylinder movement must be preceded by preliminary experiments coupled with the theory and FEM model.