• Journal of Advanced Marine Engineering and Technology
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• v.40 no.7
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• pp.587-592
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• 2016

Bellows for LNG carriers must be corrosion resistant in order to operate in seawater environments. They must also have long fatigue lives in order to withstand the expansion and contraction caused by large temperature changes and continuous vibration in extreme environments. In order to incorporate these properties into bellow design, it is important to use materials that are resistant to cold brittleness and corrosion, and maintain their optimized forming condition. The design conditions and forming methods used for bellows must be optimized in order to incorporate these characteristics. In this study, finite element analysis was used to develop cryogenic bellows, which have good mechanical strength and reliability. In addition, two different forming methods (mechanical and hydroforming) were used to design and produce bellows, in order to derive their forming condition. The height, thickness, and hardness of the convolutions of bellows produced by each method were measured and compared with each other. The results confirmed that the two forming methods produced bellows with different mechanical properties.

• Journal of Aerospace System Engineering
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• v.16 no.6
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• pp.99-105
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• 2022

This paper studied the mechanical characteristics of boom structures by verifying the modeling method of representing unit cells of triaxial woven fabric (TWF) composites. The modeling of the representative unit cell obtained the ABD matrix by analysing the behaviour of tensile, shear, bending, and torsion using the periodic boundary conditions for the beam element. This study aimed to validate the ABD matrix by comparing the tensile analysis output from a finite element program with the experimental results from an MTS 810 machine. Additionally, the mechanical characteristics of a TWF composite boom structure were determined through bending analysis and experiments. The findings of this research are expected to be beneficial for developing structures using TWF composites.

• Transactions of the Korean Society of Mechanical Engineers
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• v.14 no.4
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• pp.953-959
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• 1990

본 연구에서는 임의의 순간에서 난류유동장의 난류구조를 해석하기 위하여 Lumley의 특성 에디 분배법을 이용하였다. 이때 난류구조의 해석은 비등질성의 K-L 전개와 등질성의 푸리에 전개로 표현하여 그 수렴성, 레이놀즈 수의 영향 등 여러가지 특성을 연구하였다. 본 연구에서 선정한 비등질성 난류유동장은 Chambers등이 연구 한 랜덤력을 갖는 Burgers 방정식을 수치적으로 풀어서 얻었다. 이와 같은 난류유동 장을 K-L전개와 푸리에 전개로 표현할 때에 수렴성은 레이놀즈 수가 서로 다르고 또한 전개항의 수가 다를 때에 RMS 오차를 가지고 비교하였다.여기서 푸리에 전개 계수 들은 Galerkin 방법으로 구하였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.37 no.2
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• pp.131-138
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• 2009

Analytical modal verification is considered as the process to provide an acceptable description of the subject structure's behaviour. In general, results of original analytical model are different with actual structure results to uncertainty like non-linearity of material, boundary and modified shape, etc. In this paper, the dynamic model of glider's wing is correlated with static deformation and vibration test results by goal-attainment method, multi-objects optimization technique. The structural responses are predicted by using finite element method and optimization is carried out by using the SQP(sequential quadratic programming) method which is widely used in the constrained nonlinear optimization problem. The MAC(Modal Assurance Criterion) is used to modify the mode shapes and quantify the similarity.

• Composites Research
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• v.20 no.4
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• pp.42-50
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• 2007

This paper describes the results of experiments and numerical simulation studies on the low-velocity impact damage of two different sandwich composite panels for application to bodyshell and floor structure of the BIMODAL tram vehicle. Square test samples of 100mm sides were subjected to low-velocity impact loading using an instrumented testing machine at four impact energy levels. Part of this work presented is focused on the finite element analysis of low-velocity impact response onto a sandwich composite panels. It is based on the application of explicit finite element (FE) analysis codes LS-DYNA 3D to study the impact response of sandwich structures under low-velocity impact conditions. Material testing was conducted to determine the input parameters for the metallic and composite material model, and the effective equivalent damage model for the orthotropic honeycomb materials. Numerical and experimental results showed a good agreement for damage area and the depth of indentation of sandwich composite panels created by the impact loading.

• Journal of the KSME
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• v.25 no.3
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• pp.216-224
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• 1985

최근에는 온라인 시스템(on-line system)에 의하여 난류의 신호를 직접 신호분석기에서 받아 분석하여 컴퓨터에 의해 데이터를 처리하고, 풀롯터(plotter)에 의해 도시함으로서 유동의 특성을 통계학적인 방법으로 해석해 나가고 있다. 본 해설에서는 온라인시스템에 의한 난류의 통계 학적 측정방법과 기본적인 이론 및 측정도시에 예를 제시하고자 한다.

• Journal of the KSME
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• v.29 no.3
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• pp.270-278
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• 1989

최근 탄소성체의 소성불안정 현상과 소성 변형집중화에 의한 연성파괴 거동의 해석에 유력한 수단으로 인식되고 있는 대변형 탄소성유한 요소법의 정식화에 대하여 소개하였다. 또한 이 유한요소법에 의한 각종 소성불안정 현상의 해석에 있어서 구성관계식의 선택은 매우 중요한 의미를 갖고 있어 자주 이용되고 있는 대표적인 구성식의 특성에 대해서 논하였다.

• Proceedings of the Korean Society for Agricultural Machinery Conference
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• 2002.02a
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• pp.9-14
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• 2002

트랙터용 전후진 파워시프트 변속기의 개발을 위해서는 사용조건, 설계 조건에 맞는 유압제어 시스템 설계가 중요하며, 이를 위해서는 해석적 방법을 통하여 변속시 발생하는 클러치 흡수동력, 입출력 토크, 가속도와 저크 등에 대한 고찰이 필요하다고 판단된다.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2004.05a
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• pp.142-142
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• 2004

박막으로 표면처리한 다양한 강판이 자동차 차체와 부품, 가전제품 등의 제조를 위해 여러 가지 판재 성형공정에 적용되고 있으나, 제품 개발기간과 비용 감소, 성형과정에서 표면 코팅층의 특성 변화로 인해 성형성 열화와 성형불량을 줄이면서, 제품의 고정밀화, 고품질화를 실현하기 위해서는 코팅층에 대한 기계적 특성과 마찰거동을 명확히 규명하는 것이 반드시 필요하다 현재 나노 마이크로 수준인 코팅층의 기계적 물성치를 측정하기 위해 가장 널리 사용되는 방법은 나노 인덴테이션이다.(중략)

• Composites Research
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• v.21 no.1
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• pp.22-29
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• 2008

This paper presents the evaluation of crashworthiness and rollover characteristics of low-floor bus vehicles made of aluminum honeycomb sandwich composites with glass-fabric epoxy laminate facesheets. Crashworthiness and rollover analysis of low-floor bus was carried out using explicit finite element analysis code LS-DYNA3D with the lapse of time. Material testing was conducted to determine the input parameters for the composite laminate facesheet model, and the effective equivalent damage model for the orthotropic honeycomb core material. The crash conditions of low-floor bus were frontal accident with speed of 60km/h. Rollover analysis were conducted according to the safety rules of European standard (ECE-R66). The results showed that the survival space for driver and passengers was secured against frontal crashworthiness and rollover of low-floor bus. Also, The modified Chang-Chang failure criterion is recommended to predict the failure mode of composite structures for crashworthiness and rollover analysis.