• Electrical & Electronic Materials
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• v.3 no.3
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• pp.187-194
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• 1990

광자기 메모리용 재료인 비정질 TbFe 박막을 대상으로 열자기 기록시 박막에 분포하는 온도와 이때 만들어지는 bit의 크기간에 상호관련성을 조사하였다. 레이저 조사에 의해 가열된 박막의 온도분포는 유한요소법을 이용한 열전달 해석에 의해 계산하였다. 레이저 가열종료 직전 박막 면에 분포하는 온도 contour로 부터 bit 크기를 예측하였다. 여기서 bit 크기는 온도 상승에 따라 보자력이 약화되어 외부자계와 박막반자장의 합력이 역자구를 만들어 준다고 가정하여 이 경계가 되는 온도(Tcrit)로 이루어지는 등온선의 크기로부터 정하였다. 열자기 기록 실험으로부터 기록 bit의 크기(Dmeas.)을 측정하여 레이저조사조건별로 예측한 bit크기(Dpred.)와 비교하였다. 특히, 레이저 pulse시간 변화에 따른 여러온도의 등온선 contour 직경변화를 조사하여 실측한 bit크기와 비교 검토함으로써 bit형성에 미치는 온도분포의 영향을 조사하였다. 이 결과 레이저 pulse시간이 길어지거나 레이저 power가 상대적으로 작을때 실측한 bit크기가 예측된 bit크기보다 커지는 것으로 나타났으며 이는 Tcrit 온도구배가 완만해질수록 bit경계가 되는 온도가 낮아지는 것으로 해석된다.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2005.11a
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• pp.147-150
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• 2005

The torsion beam axle type is widely used in the rear suspension for small passenger car because of low cost, good performance and etc. The FE and dynamic analysis using the computer are very helpful for the efficiency of the torsion beam design. First of all, the reliability on the computational model must be verified for the analysis. In this study, The FE model of the torsion beam was verified according to comparison with he test data. And after making the flexible body using the FE model, the dynamic characteristic of the tubular type torsion beam axles was compared with that of the V-beam type.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.14 no.4
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• pp.481-494
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• 2001

An enhanced degenerated shell finite element (FE), which has been developed for inelastic analysis of reinforced concrete structures is described in this paper. Generally, Reissner-Mindlin (RM) assumptions are adopted to develop the degenerated shell FE so that transverse shear deformation effects is considered. However, it is found that there are serious defects such as locking phenomena in RM degenerated shell FE since the stiffness matrix has been overestimated in some situations. As remedies of locking phenomena, reduced integration, incompatible mode and assumed strain method have been used. Especially, the assumed strain method has been successfully used in many FEs. But contrarily, there is a few investigation on the performance of the assumed strains in the inelastic analysis of concrete structures. Therefore, shell formulation is provided in this paper with emphasis on the terms related to the stiffness matrix based on assumed strain method and microscopic concrete material model. Finally, the performance of the present shell element is tested and demonstrated with several numerical examples. From the numerical tests, the present result shows a good agreement with experimental data or other numerical results.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.22 no.3
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• pp.289-296
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• 2009

Natural frequency is a key parameter to determine the seismic and wind loading of tall flexible structures, and to assess the wind-induced vibration for serviceability check. In this study, natural frequencies and associated mode shapes were obtained from measured acceleration data and system identification technique. Subsequently, finite element(FE) models for a tall reinforced concrete buildings were built using a popular PC-based finite element analysis program and calibrated to match their natural frequencies and mode shapes to actual values. The calibration of the FE model included: 1) compensation of modulus of elasticity considering the mix design strength, 2) flexural stiffness of floor slabs, and 3) major non-structural components such as plain concrete walls. Natural frequencies and mode shapes from the final FE model showed best agreement with the measured values.

• Composites Research
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• v.31 no.1
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• pp.37-41
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• 2018

The aim of the current work is to characterise a piecewisely-integrated composite bumper beam based on the IIHS bumper crash protocol. IIHS bumper crash FE analysis for an aluminium type bumper beam was carried out to get the information about the dominant loading types at several regions in the bumper beam during crash. In the meantime, robust stacking sequences against tension and compression have been searched for using FE analysis of a coupon type model. After determining most effective stacking sequences for tension and compression, three-point bending simulation was preliminarily carried out to investigate the combination performance of them. Finally, IIHS bumper crash FE analysis for the piecewisely-integrated composite bumper beam, which consisted of the combination of tension effective stacking sequence and compression efficacious stacking sequence, was conducted and the result was compared with other types of composite bumper beams. It was found that the newly suggested piecewisely-integrated composite bumper beam showed superior crashworthy behaviour to those of uni-modal stacking sequence composite bumper beams.

• Transactions of Materials Processing
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• v.15 no.4 s.85
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• pp.319-325
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• 2006

The laser forming process is a new flexible forming process without forming tools and external force, which is applied to various fields of industry. Especially, applications of the laser forming process focused on cutting, welding and marking process. In this paper, the laser bending process of sheet metal which is heated by laser beam and formed by internal stress is simulated by using thermo elastic-plastic analysis model. Based on the result of FE-analysis, the laser bending machine is made to obtain reliable data for sheet bending. Under the same condition as FE-analysis, the laser bending experiment has been performed to ver 펴 the result of FE-analysis and good agreement has been obtained between FE-analysis and experiments. Additional laser bending experiments have been performed to evaluate the laser bending machine.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2007.11a
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• pp.213-214
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• 2007

• Proceedings of the Korean Magnestics Society Conference
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• 1999.04a
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• pp.30-31
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• 1999

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2009.06a
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• pp.393-394
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• 2009

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2009.06a
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• pp.1071-1072
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• 2009