• Transactions of the Korean Society of Mechanical Engineers
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• v.16 no.8
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• pp.1519-1529
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• 1992

A stepped specimen which is subjected to step loading is modeled to study the initiation and growth of adiabatic shear band using explicit time integration finite element code. The material model for specimen includes effects of thermal softening, strain hardening and strain rate hardening. Various mesh sizes are tested to check whether they are small enough to model highly localized discontinuous phenomena reasonably well. It is shown that the number of adiabatic shear band depends on impact velocity and it is also shown that the initiation and growth of adiabatic shear band inversely depends on prescribed velocity at the top of specimen.

• Transactions of the Korean Society of Mechanical Engineers
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• v.8 no.6
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• pp.599-603
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• 1984

Field equations describing the effective behavior of general heterogeneous media are derived from the integral balance relations through the methods of distribution and convolution.

• Composites Research
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• v.36 no.2
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• pp.117-125
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• 2023

This paper proposes a new finite element formulation based on enhanced first-order shear deformation theory including the transverse normal strain effect via the mixed formulation (EFSDTM-TN) for the effective thermo-mechanical analysis of laminated composite structures. The main objective of the EFSDTM-TN is to provide an accurate and efficient solution in describing the thermo-mechanical behavior of laminated composite structures by systematically establishing the relationship between two independent fields (displacement and transverse stress fields) via the mixed formulation. Another key feature is to consider the thermal strain effect without additional unknown variables by introducing a refined transverse displacement field. In the finite element formulation, an eight-node isoparametric plate element is newly developed to implement the advantage of the EFSDTM-TN. Numerical solutions for the thermo-mechanical behavior of laminated composite structures are compared with those available in the open literature to demonstrate the numerical performance of the proposed finite element model.

• Proceedings of the KAIS Fall Conference
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• 2011.05b
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• pp.989-992
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• 2011

삼원 촉매는 주로 코제라이트 세라믹으로 제작되는 다공성 부품이다. 그러나 코제라이트 세라믹은 열적충격온도가 낮아 엔진의 혼합기가 농후한 경우 삼원촉매의 열적 내구성이 급격히 떨어져 내구 수명을 제대로 만족시키지 못하는 차량이 급격히 증가하고 있다. 따라서 본 논문은 유한요소법으로 구한 SiC 세라믹 재료의 등가 물성치를 기초로 SiC 세라믹 촉매 담체의 기계적 물성치를 유한요소해석용시험편으로 구한 뒤 SiC 세라믹 촉매담체가 실차에 설치될 경우의 열피로 성능에 대하여 평가하였다.

• Proceedings of the KIPE Conference
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• 2018.11a
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• pp.137-138
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• 2018

본 논문은 단일 배터리의 발열량 추정을 위한 전기-열적 해석을 수행하였다. 셀의 물리적 특성, SOC별 저항에 중점을 두어 발열량 추정을 하였다. 실험과 시뮬레이션을 비교하여 제시한 모델과 발열 저항의 의미를 확립 및 검증하며 단일 배터리의 방전구간 발열량을 추정하였다.

• Journal of Power System Engineering
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• v.5 no.1
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• pp.73-79
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• 2001

정전기력을 이용하는 마이크로가속도계 센서는 단결성 실리콘 SOI(Silicon On Insulator) 웨이퍼의 기판에 절전재료 적층과 등방성 및 이방성 부식공정으로 제작한다. 마이크로가속도 센서 개발에는 3차원 미소구조체의 제작공정에서 가열 및 냉각공정의 온도구배로 야기되는 포핑업과 같은 열변형 해석이 최적 형상설계에 중요한 요건이다. 본 연구에서는 양자역학적 현상인 턴널링전류 원리로 승용차 에어백의 검침부 역할을 하는 마이크로가속도 센서의 제조공정에서 소착현상을 방지하는 부가 비임과 턴널갭의 FIB 절단가공과 백금 적층공정의 열적 거동을 해석한다. 마이크로머시닝 공정에서 온도의존성을 고려하여 연성해석하고 유한요소법의 상용코드인 MARC K6.1로 분석한 결과를 단결정 실리콘 웨이퍼로 가공하는 마이크로가속도 센서의 최적공정 및 형상설계를 위한 기초자료로 활용될 수 있을 것으로 기대된다.

• Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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• 2008.06a
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• pp.243-244
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• 2008

점점 전송 기술이 발달함에 따라, 고속/대용량의 광 연결 기술이 많이 응용되고 있다. 소자들 또한 이러한 광 신호를 받기에 적합한 형태가 필요하다. 따라서 본 논문에서는, 미리 설계한 광 신호로 동작하는 PZT 액추에이터의 동작 범위와 변위를 FEM 시뮬레이션(Finite Element Method Simulation)을 통해 해석해 보니 10V 전압에서 532nm의 변위를 확인할 수 있었고, 또한 열적, 기계적, 전기적 해석을 통하여 차후 제작에 감안할 점들을 찾아내는데 주안점을 두었다.

• Journal of Aerospace System Engineering
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• v.17 no.4
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• pp.1-9
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• 2023

Recently, as Synthetic Aperture Radar (SAR), communication, and signal surveillance missions of spacecraft have become more advanced, research has been actively conducted on the deployable large mesh antenna system with excellent storage efficiency compared to the deployment area, and light weight. Deployable Mesh antennae are characterized by an increase in the number of Openings Per Inch (OPI), which is a measure of mesh weaving density as the mission frequency band increases, and this OPI change directly affects the thermal optical properties of the mesh antenna, so research on this is required. In this paper, to verify the thermal relationship between the optical properties of the mesh and antenna reflector, thermal sensitivity analysis between the mesh and the antenna reflector is performed by in-orbit thermal analysis with various optical characteristics of the mesh based on existing overseas research cases. In addition, the temperature gradient effect of the mesh reflector is analyzed.

• Journal of the Korean Institute of Gas
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• v.7 no.3 s.20
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• pp.58-64
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• 2003

This paper presents design safety analysis of pressure vessels. The gas pressure and thermal loads are applied to the pressure vessel simultaneously. In this study, ASME Sec. VIII Div. 2 code was accepted for the safety design of high-pressure vessel. And this result was analyzed using a coupled thermal-mechanical FEM analysis technique. The FEM computed result shows that ASME design code may not guarantee for combined loads of high gas pressure and thermal loads. And solid pressure vessel may be safe compared to other pressure vessels with supporting rings round the cylinder body.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.14 no.12
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• pp.6106-6113
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• 2013

Automotive three-way catalyst substrate has a cordierite ceramic honeycomb structure. The substrate in the high engine speed range doesn't satisfy the design fatigue life due to the low mechanical properties of cordierite ceramic. SiC ceramic has higher mechanical properties than cordierite ceramic. If the automotive three-way catalyst substrate is made from the SiC ceramic honeycomb structure, the substrate can be prevented from premature failure. In this study, the mechanical properties of SiC ceramic honeycomb substrate were estimated by FEA. The FEA results indicated that the MOR and elastic modulus for the SiC ceramic honeycomb substrate was much higher than those for the cordierite ceramic honeycomb substrate.