• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 춘계학술대회논문집C
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• pp.572-579
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• 2001

본 연구에서는 유한요소해석을 통한 와이어 방전가공기의 설계검증을 위하여 두 모델을 선정하여 CAD 패키지 I-DEAS를 이용하여 3차원 유한 요소모델을 모델링한 후 상용 유한요소해석코드인 ABAQUS로 각 모델의 가공위치에 따른 해석을 수행하였다. JW-35A와 JW-60A 두 모델의 상호 비교 타당성 여부를 확인하기 위하여 ${\eta}-factor$ 개념을 이용하였다. 이어 공리적 설계 개념을 도입하여 오차보정을 위한 설계변수들의 선택과 방법이 적절함을 보이고 두 모델의 유한요소해석 결과를 상호 비교하여 구조물의 설계를 검증하고 변형 예측식을 유도하였다. 본 연구를 통해 유도된 변형 예측식 (5)-(6) 형태의 접근방법은 비단 방전가공기 뿐만 아니라 이와 유사한 형태의 공작기계에도 적용 할 수 있을 것이다.

• Structural Engineering and Mechanics
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• 제53권5호
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• pp.997-1016
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• 2015

The contribution of tensioned concrete between cracks (tension-stiffening) cannot be ignored when analysing deformation of reinforced concrete elements. The tension-stiffening effect is crucial when it comes to adequately estimating the load-deformation response of steel reinforced concrete and the more recently appeared fibre reinforced polymer (FRP) reinforced concrete. This paper presents a unified methodology for numerical modelling of the tension-stiffening effect in steel as well as FRP reinforced flexural members using the concept of equivalent deformation modulus and the smeared crack approach to obtain a modified stress-strain relation of the reinforcement. A closed-form solution for the equivalent secant modulus of deformation of the tensioned reinforcement is proposed for rectangular sections taking the Eurocode 2 curvature prediction technique as the reference. Using equations based on general principles of structural mechanics, the main influencing parameters are obtained. It is found that the ratio between the equivalent stiffness and the initial stiffness basically depends on the product of the modular ratio and reinforcement ratio ($n{\rho}$), the effective-to-total depth ratio (d/h), and the level of loading. The proposed methodology is adequate for numerical modelling of tension-stiffening for different FRP and steel reinforcement, under both service and ultimate conditions. Comparison of the predicted and experimental data obtained by the authors indicates that the proposed methodology is capable to adequately model the tension-stiffening effect in beams reinforced with FRP or steel bars within wide range of loading.

• 한국HCI학회논문지
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• 제2권2호
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• pp.19-26
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• 2007

이 논문에서는 증강현실을 이용하여 디포머블(Deformable)한 3차원의 도자기 모델을 손을 이용하여 자연스러우면서도 직관적으로 변형시키고, 이를 실제 물체들과 같이 디스플레이 해 줌으로써 실재감을 느낄 수 있는 새로운 시스템을 제안한다. 제안된 시스템에서는 값비싸면서도 거추장스러운 장비를 사용하지 않고도 카메라와 마커의 상대적인 위치를 통해서 손의 위치를 알아내게 되고, 일반적으로 물체를 변형시킬 때 사용하는 손의 움직임을 본떠 6가지 형태의 모델링 인터페이스 및 버튼형 인터페이스를 제공한다. 그리고 실시간으로 변형된 모델에 대한 결과를 증강현실을 이용하여 디스플레이 해 주는 방법을 통해서 물체의 크기 및 모양을 좀 더 실재감 있게 느낄 수 있게 한다. 이러한 방법은 비단 도자기뿐만 아니라 다양한 분야에 활용 가능하며, 보통 컴퓨터가 있는 집에 화상카메라가 하나 정도는 있다는 점에서 교육적인 용도로써의 활용 가능성이 상당히 크다 할 수 있을 것이다.

• International Journal of Naval Architecture and Ocean Engineering
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• 제9권3호
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• pp.315-325
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• 2017

The design dimension may not be satisfactory at the final stage due to the welding during the assembly stage, leading to cutting or adding the components in large structure constructions. The productivity is depend on accuracy of the welding quality especially at assembly stage. Therefore, it is of utmost importance to decide the component dimension during each assembly stage considering the above situations during the designing stage by exactly predicting welding deformation before the welding is done. Further, if the system that predicts whether welding deformation is equipped, it is possible to take measures to reduce deformation through FE analysis, helping in saving time for correcting work by arresting the parts which are prone to having welding deformation. For the FE analysis to predict the deformation of a large steel structure, calculation time, modeling, constraints in each assembly stage and critical welding length have to be considered. In case of fillet welding deformation, around 300 mm is sufficient as a critical welding length of the specimen as proposed by the existing researches. However, the critical length in case of butt welding is around 1000 mm, which is far longer than that suggested in the existing researches. For the external constraint, which occurs as the geometry of structure is changed according to the assembly stage, constraint factor is drawn from the elastic FE analysis and test results, and the magnitude of equivalent force according to constraint is decided. The comparison study for the elastic FE analysis result and measurement for the large steel structure based on the above results reveals that the analysis results are in the range of 80-118% against measurement values, both matching each other well. Further, the deformation of fillet welding in the main plate among the total block occupies 66-89%, making welding deformation in the main plate far larger than the welding deformation in the longitudinal and transverse girders.

• 대한조선학회논문집
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• 제49권6호
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• pp.528-533
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• 2012

Flexible composite propellers are subject to large deformation under heavy loading, and hence the hydrodynamic performance of deformed propeller might deviate from that of the metallic propeller under negligible deformation. To design the flexible propeller, it is therefore necessary to be able to evaluate the structural response of the blades to the hydrodynamic loadings, and then the influence of the blade deformation upon the hydrodynamic loadings. We use the lifting-surface-theory-based propeller analysis and design codes in solving the hydrodynamic problem, and the finite-element-method program formulated with 20-node iso-parametric solid elements for the analysis of the structural response. The two different hydrodynamic and structural programs are arranged to communicate through the carefully-designed interface scheme which leads to the derivation of the geometric parameters such as the pitch, the rake and the skew distributions common to both programs. The design of flexible propellers, suitable for manufacturing, is shown to perform the required thrust performance when deformed in operation. Sample design shows the fast iteration scheme and the robustness of the design procedure of the flexible propellers.

• Design & Manufacturing
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• 제6권1호
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• pp.12-17
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• 2012

In order to produce high-quality optical components, aspheric lenses have been widely applied in recent years. An aspheric lens consists of aspheric surfaces instead of spherical ones, which causes difficulty in the design process as well as the manufacturing procedure. Although injection molding is widely used to fabricate optical lenses owing to its high productivity, there remains lots of difficulty to determine appropriate mold design factors and injection molding parameters. In the injection molding fields, computer simulation has been effectively applied to analyze processes based on the shell analysis so far. Considering the geometry of optical lenses, a full-3d simulation based on solid elements has been reported as a reliable approach. The present work covers three-dimensional injection molding simulation and relevant deformation analysis of an injection molded plastic lens based on 3d solid elements. Numerical analyses have been applied to the injection molding processes of three aspheric lenses for an image sensing module of a mobile phone. The reliability of the proposed approach has been verified in comparison with the experimental results.

• 한국CDE학회논문집
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• 제15권6호
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• pp.411-417
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• 2010

In this paper, the boom of a floating crane is modeled as a 3-dimensional elastic beam in order to analyze the dynamic response of the crane and its cargo. The boom is divided into more than two elements based on finite element formulation, and deformation of each element is expressed in terms of shape matrix and nodal coordinates. The equations of motion for the elastic boom consist of a mass matrix, a stiffness matrix, and a quadratic velocity vector that contains the gyroscopic and Coriolis forces. The size and complicity of the matrices increase in proportion with the number of elements. Therefore, it is not possible to derive the equations of motion explicitly for different number of elements. To overcome this difficulty, matrices for one 3-dimensional element are expressed with elementary sub-matrices. In particular, the quadratic velocity vector is derived as a product of a shape matrix and a 3-dimensional rotation matrix. By using the derived matrices, the equations of motion for the multi-element boom are automatically constructed. To verify the implementation of the elastic boom based on finite element formulation, we simulated a simple vibration of the elastic boom and compared the average deformation with the analytic solution. Finally, heave motion of the floating crane and surge motion of the cargo are presented as application examples of the elastic boom.

• Earthquakes and Structures
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• 제13권1호
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• pp.59-66
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• 2017

Modern seismic codes rely on performance-based seismic design methodology which requires that the structures withstand inelastic deformation. Many studies have focused on the inelastic deformation ratio evaluation (ratio between the inelastic and elastic maximum lateral displacement demands) for various inelastic spectra. This paper investigates the inelastic response spectra through the ductility demand ${\mu}$, the yield strength reduction factor $R_y$, and the inelastic deformation ratio. They depend on the vibration period T, the post-to-preyield stiffness ratio ${\alpha}$, the peak ground acceleration (PGA), and the normalized yield strength coefficient ${\eta}$ (ratio of yield strength coefficient divided by the PGA). A new inelastic deformation ratio $C_{\eta}$ is defined; it is related to the capacity curve (pushover curve) through the coefficient (${\eta}$) and the ratio (${\alpha}$) that are used as control parameters. A set of 140 real ground motions is selected. The structures are bilinear inelastic single degree of freedom systems (SDOF). The sensitivity of the resulting inelastic deformation ratio mean values is discussed for different levels of normalized yield strength coefficient. The influence of vibration period T, post-to-preyield stiffness ratio ${\alpha}$, normalized yield strength coefficient ${\eta}$, earthquake magnitude, ruptures distance (i.e., to fault rupture) and site conditions is also investigated. A regression analysis leads to simplified expressions of this inelastic deformation ratio. These simplified equations estimate the inelastic deformation ratio for structures, which is a key parameter for design or evaluation. The results show that, for a given level of normalized yield strength coefficient, these inelastic displacement ratios become non sensitive to none of the rupture distance, the earthquake magnitude or the site class. Furthermore, they show that the post-to-preyield stiffness has a negligible effect on the inelastic deformation ratio if the normalized yield strength coefficient is greater than unity.

• 한국가스학회지
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• 제19권1호
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• pp.23-27
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• 2015

본 연구에서는 원통형 중공롤러의 응력과 변형거동 안전성을 FEM으로 해석하고, 그 계산결과를 기초로 과도 설계 여부를 고찰하였다. 중공롤러의 강도에 관련된 응력해석 결과에 따르면, 중공롤러를 지지하는 베어링을 설치한 인근에서 발생한 최대응력 39.8MPa은 구조용 강재의 항복강도인 250MPa 대비 15.9% 수준으로 과도한 설계로 평가될 수 있다. 또한, 원통형 중공롤러의 전체 길이 대비 중간 스팬부에서 발생한 최대 변위량 0.032mm는 중공롤러의 전체 길이와 두께에 견주어 볼 때 충분히 안전하다할 수 있다. 결국, 강도와 변형거동에 대한 FEM 해석결과에 의하면, 현재의 원통형 중공롤러 FEM 해석모델은 과도하게 설계되었다고 분석된다.

• 한국정밀공학회지
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• 제30권4호
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• pp.434-441
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• 2013

Bending motion has been used in the surgical instruments with bending structures and tendon mechanisms. A simplified bending angle amplification ratio between the proximal and distal bending joint was derived in this article. The bending structure of disk and rib in the proximal joint was analyzed based on finite element method with an emphasis on the circumferential uniformity of bending stiffness. Regarding the distal joint, optimal design and sensitivity analysis was done with four design variables of outer and inner diameter, rib height and rib width while maximizing the deformation under the stress distribution below the yield stress. Outer diameter and rib width are most critical to maximum deformation as the outer diameter and inner diameters are so to maximum equivalent stress.