• Proceedings of the KIEE Conference
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• 2011.07a
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• pp.912-913
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• 2011

본 논문은 Yoke 형상 변화에 따른 EV-Relay 구동 액츄에이터의 동작특성에 대해 연구하였다. 요크는 기본 형상을 포함하여 3가지 형태이며, 각 형상에 대해 유한요소해석으로 동작특성을 계산하였다. 계산시간 단축을 위해 2차원 축대칭 모델을 이용하였고, 기계적 부하를 동작특성 계산과정에 포함하여 실제동작상태와 유사하게 표현하였다. 마지막으로, 요크 형상에 따른 3가지 모델의 계산결과를 비교하여 기존 모델보다 형상이 변화된 모델의 동작특성이 개선되었음을 확인하였다.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.15 no.3
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• pp.399-407
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• 2002

A three-dimensional method of analysis is presented for determining the free vibration frequencies and mode shapes of hollow bodies of revolution (i.e., thick shells), not limited to straight line generators or constant thickness. The middle surface of the shell may have arbitrary curvatures, and the wall thickness may vary arbitrarily. Displacement components$U_\Phi, U_z, U_\theta$ in the meridional, normal and circumferential directions, respectively, are taken to be sinusoidal in time, periodic in$\theta$, and algebraic polynomials in the$\Phi$and z directions. Potential(strain) and kinetic energies of the entire body are formulated, and upper bound values of the frequencies are obtained by minimizing the frequencies. As the degrees of the polynomials are increased, frequencies converge to the exact values. Novel numerical results are presented for two types of thick conical shells and thick spherical shell segments having linear thickness variations. Convergence to four digit exactitude is demonstrated for the first five frequencies of both types of shells. The method is applicable to thin shells, as well as thick and very thick ones.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.34 no.5
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• pp.567-573
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• 2010

In this study, we evaluated the structural integrity and weight of a rocket motor with a torispherical dome by size optimization. Size optimization was achieved by first-order and sub-problem methods, using the Ansys Parametric Design Language (APDL). For rapid design verification, a modified 2D axisymmetric finite-element model was used, and the bolt pre-tension load was expressed as function of the ratio of the cross-sectional area. The thickness of the dome and the cylindrical part of the rocket motor were selected as the design parameters. Our results showed that the weight and structural integrity of the rocket motor at the initial design stage could be determined more rapidly and accurately with the modified 2D axisymmetric finite-element model than with the 3D finite-element model; further, the weight of the rocket motor could be saved to maximum of 17.6% within safety limit.

• Journal of the Korean Society of Visualization
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• v.12 no.3
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• pp.21-25
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• 2014

Optical distortion of experimental results can be found in many studies. Thus, a method of the optical correction for visualization of an axisymmetric droplet was developed in this study. The correction method was derived to extract refracted vectors. In order to obtain the refracted vectors, a projection vector and a normal vector should be calculated. Then, a distortion distance can be found by the calculated refracted vector and Snell's law. The developed method was also verified by the simulation and the experimental results to apply for a liquid droplet which was formed at a nozzle tip.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2011.11a
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• pp.565-569
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• 2011

A two-dimensional thermal response and ablation analysis code for predicting charring material ablation and shape change on solid rocket nozzle is presented. For closing the problem of thermo-structural analysis, Arrhenius' equation and Zvyagin's ablation model are used. The moving boundary problem are solved by remeshing-rezoning method. For simulation of complicated thermal protection systems, this method is integrated with a three-dimensional finite-element thermal and structure analysis code.

• Journal of computational fluids engineering
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• v.2 no.2
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• pp.35-43
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• 1997

An efficient inverse method for 1.he supersonic/hypersonic axisymmetric body design is developed for the parabolized Navier-Stokes equations. The developed method is examined numerically for three extreme testcases in the supersonic(M/sub ∞/=3.0) and hypersonic(M/sub ∞/=6.28) speeds. The first one is a negative pressure distribution near a vacuum pressure and the second one is a positive pressure distribution over the whole region of the body. The last one is the case of abrupt change of pressure distribution to zero in the forward region of the body. These testcases show the robustness of the method. By introducing a regular-falsi method and by using a not-fully converged inverse solution, the convergence behavior was greatly improved.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 1995.04a
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• pp.184-189
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• 1995

자동차 흡배기계의 음향성능 해석에 일반적으로 사용되고 있는 방법은 평면과 이론에 의한 1차원적인 해석방법이다. 그러나 관심 주파수 대역이 높거나 대상물의 형상이 복잡한 경우, 또는 내부에 흡음재가 부착되어 있는 경우에는 이러한 1차원 해석으로는 만족할만한 결과를 얻을 수 없으므로 경계요소법(BEM), 유한요소법(FEM) 등과 같은 수치해석 방법이 이용되고 있다. 본 연구에서는 축대칭 단순팽창형, 연장관형, 다공형등 반사형 소음기와 흡음형 소음기의 음향성능을 해석하기 위한 경계요소법 프로그램을 개발하고, 소음기 성능의 주파수 특성을 구하여 실험결과 및 1차원 해석 결과와 비교 고찰하였다.

• Journal of the Korean Geotechnical Society
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• v.17 no.4
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• pp.7-14
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• 2001

구조물 하중에 의한 점성토 지반의 침하량을 보다 정확하게 평가하기 위해서는 지반 내의 흙요소가 경험하는 실제적인 응력경로와 이에 따른 변형양상이 적절하게 고려되어야만 한다. 따라서 본 연구에서는 축대칭 조건의 다양한 응력경로를 따라 발생하는 정규압밀 점성토의 변형 거동을 고찰한 기존의 실험적 연구결과를 바탕으로 응력경로법에 근거한 보다 간편하고 합리적인 침하량 평가기법을 제시하였다. 또한 본 연구에서는 제시된 평가기법을 기존의 1차원적인 침하량 평가기법들과 함께 실제와 유사한 조건을 가지는 가상지반의 침하량 산정에 적용해 보았으며, 동일한 조건에 대해 소성모델(MCC 모델)과 혼합압밀이론에 바탕을 둔 유한요소해석을 실시하였다. 그리고 이를 통해 얻어진 결과들을 비교.분석함으로써 기존 평가기법들의 문제점과 한계를 명확히 제시하였으며, 응력증분 평가방법이 침하량 평가에 미치는 영향을 분석하였다.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.21 no.6
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• pp.925-932
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• 1997

Two shear-flexible curved axisymmetric shell elements with two nodes, LCCS(linear curvature and constant strain) and CCCS(constant curvature and constant strain) are designed based on the assumed meridional strain fields and shallow shell geometry. At the element level, meridional curvature, membrane strain and shear strain fields are assumed by using polynomials and the displacement fields are obtained by integrating the assumed strain fields along the shallowly curved meridian. The formulated elements have high order displacement fields consistent with the strain field. Several test problems are given to demonstrate the performance of the two elements. Analysis results obtained reveal that the elements are very accurate in the displacement and the stress predictions.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2004.05a
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• pp.246-246
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• 2004

현재 비구면렌즈를 만들기 위해서는 다양한 방법이 있다. Glass종류의 가공시 초정밀 절삭가공기(DTM)에서 가공하거나 정밀 연삭기를 가지고 가공하게 된다. 이 과정에서 렌즈 표면에 공구 흔적이나 표면거칠기 개선을 위해 연마작업을 하게 되는데, 사용하는 장비가 폴리싱 머신이다. 축대칭인 폴리싱머신의 경우 X, Z, $\theta$로 동시 3축제어가 가능하다. 하지만 이 장비의 경우 연마에서 원하는 형상정밀도와 표면거칠기를 얻기 위해 각축들의 위치정밀도와 분해능이 높은 부품을 사용하여 기계자체가 고가라는 점이 단점으로 작용한다.(중략)