• 대한기계학회논문집
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• 제10권3호
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• pp.383-391
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• 1986

본 논문에서는 이들 기본모우드형태가 검토되었고 또한 두께효과와 비대칭성 효과에 따른 고유진동주파수, 모우드형태, 울림주파수의 변화를 수치적 해석과 실험 적 해석방법에 의해 비교검토되었다. 수치해석방법은 유한요소법으로 이용된 프로그 램은 NASTRAN 프로그램이고 모우드의 형태는 Tectronics컴퓨터그래픽을 이용하여 나타 내었다. 실험적방법은 충격햄머법과 F.F.T. 분석장치(Fast Fourier Transformation Analyzer)를 이용하였다.

• 한국소음진동공학회논문집
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• 제20권8호
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• pp.703-709
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• 2010

An analysis tool for predicting transmission loss in high speed trains based on combined use of the statistical energy analysis and the finite element methods has been proposed. The analysis utilizes a commercially available numerical solver VA ONE with imbedded NASTRAN module. The proposed analysis tool is first verified by comparing numerically predicted transmission loss of a light rail transport(LRT) structure with experimental results. The comparison shows that the numerically predicted transmission loss is similar to the experimental data. The analysis tool is then applied to the prediction of transmission loss in the high speed train(HST) currently under development. Various sub-structures such as the floor, side panel and ceiling have been numerically analyzed to predict their transmission losses. The results obtained here can be used as input data for predicting the interior noise level of the HST at design stage.

• 한국항공우주학회지
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• 제30권2호
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• pp.122-129
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• 2002

우주 구조물인 하나콤 위성본체 플래폼의 구조최적화를 수행하였다. 하나콤 위성 플래폼의 최적설계에는 다양한 우주 환경 하에서 고려하기 어려운 제한 조건들이 고려된다. 이러한 제한 조건들을 고려하기 위해서 최적화 기법인 변형 유용 방향 탐색법과 유전자 알고리즘을 유한 유소 해석 기법을 사용하는 MSC/NASTRAN과 병행하여 최적화를 수행하였다. 하나콤 위성 플래폼의 최적화는 정적해석과 동해석을 통하여 베어링 응력과 고유 진동수에 대한 제한조건을 사용하여 수행하였다. 본 연구의 수행 결과 국부 최적화 기법인 변형 유용 방향 탐색법이 전역 최적화 기법인 유전자 알고리즘에 의한 최적화 보다 좋은 결과를 얻을 수 있었다. 또한, 두 기법의 최적화 모두 응력 보다는 고유 진동수에 의한 제한 조건이 최적화에 더 큰 영향을 준다는 사실을 알게 되었다. 하나콤 위성 플래폼의 최적화를 통해서 주어진 환경에 더 적합하고 안정성 있는 플래폼의 구조최적설계를 할 수 있었다.

• 한국해양공학회지
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• 제22권5호
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• pp.132-137
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• 2008

Ship structures are subject to severe environmental loads causing appreciable hull girder bending which in turn affects the piping system attached to the main hull in the form of a displacement load. While this load may cause failure in the pipes, loops have been widely adopted as a means of preventing this failure, with the idea that they may lower the stress level in a pipe by absorbing some portion of the displacement load. But since such loops also have some negative effects, such as causing extra manufacturing cost, deteriorating the function of the pipe, and occupying extra space, the number and dimensions of the loops adopted need to be minimized. This research developed design formulas for pipe loops, modeling them as frames composed of beam elements, where not only bending but also shear deflection is taken into account. The accuracy of the proposed design formulas was verified by comparing two results respectively obtained by the proposed formulas and MSC/NASTRAN. The paper concludes with a sample example showing the efficiency of the proposed formulas.

• 한국전산구조공학회논문집
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• 제18권1호
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• pp.71-78
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• 2005

수정 시뮬레이티드어닐링은 Simulated Annealing(SA)가 확률 탐색 방법을 사용하기 때문에 수렴시간이 오래 걸리는 단점를 개선한 방법이다. 따라서 본 논문에서는 RSA와 SA을 트러스구조물과 인공위성구조물의 최적화에 적용하여 서로 비교하여 보았다. 최적화 예제로 10부재 트러스, 실제 응용예제로 인공위성구조물은 위성 상단 플랫폼과 추진모듈의 최적화를 수행하였다. 인공위성구조물의 최적화에서 응력과 고유진동수, 전단응력 등을 제한조건으로 고려하여 최적화를 수행하였다. 인공위성구조물의 최적화를 수행한 결과 RSA을 이용하여 다양한 인공위성 구조물의 최적화에 적용될 수 있음을 확인하였으며, 인공위성 구조물의 최적화에서 RSA가 SA보다 수렴속도가 향상되었음을 확인하였다.

• 대한기계학회논문집
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• 제16권10호
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• pp.1807-1815
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• 1992

본 연구에서는 적층 복합재 원통쉘의 동적특성을 검토한다. 복합재료 원통 쉘의 설계에서 주요 관심 대상인 직교이방성 변수가 진동특성과 어떤 관계를 갖는지 알아보기 위하여 직교이방성이론으로 한정시켜 해석하였다. 지배방정식은 면내관성 항을 고려한 Donnell 운동방정식을 사용하며, 진동수방정식은 Rayleigh-Ritz법을 이용 하여 유도하였다. 임의의 경계조건에 적용될 수 있도록 보특성함수를 사용하여 고유 진동수를 간단히 구하였다. 기존의 연구자들이 채용한 복합재료의 물성치들과 복합 재 원통쉘의 고유진동수사이에 어떤관계가 있는지 규명하도록 하였다.

• 한국공작기계학회:학술대회논문집
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• 한국공작기계학회 2002년도 춘계학술대회 논문집
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• pp.357-362
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• 2002

Most of battery industries are growing explosively as a core strategy industry for the development of the semi-conductor, the LCD, and the mobile communication device. In this thesis, dynamic characteristics of the steel can labeling machine on the automatic cell assembly line are studied. Dynamic characteristic analysis consists of dynamic behavior analysis and finite element analysis and is necessary for effective design of machines. In the dynamic behavior analysis, the displacement, velocity, applied force and angular velocity of each components are simulated according to each part. In the FEA, stress analysis, mode analysis, and frequency analysis are performed for each part. The results of these simulations are used for the design specification investigation and compensation for optimal design of cell manufacturing line. Therefore, Virtual Engineering of the steel can labeling machine on the automatic cell assembly line systems are modeled and simulated. 3D motion behavior is visualized under real-operating condition on the computer window. Virtual Prototype make it possible to save time by identifying design problems early in development, cut cost by reducing making hardware prototype, and improve quality by quickly optimizing full-system performance. As the first step of CAE which integrates design, dynamic modeling using ADAMS and FEM analysis using NASTRAN are developed.

• 한국생산제조학회지
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• 제21권4호
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• pp.608-612
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• 2012

To reduce these costs and time by finite element analysis program has been much research (3~4). At virtual CAE program as like Abaques, Ansys, Ls-dyna and Nastran, the input data of material is got bellow coupon test. In case of carbon composite, it is also put in lamina/laminate properties. There have big problem. If you want to simulate FW(filament winding or wind blade) how do you input material data. Each area of FW is different stacking conditions. It's too hard that each area is tested for inputting lamina or laminate properties. The composite structure increasing load is applied occurred as the matrix dependence of the crack-induced nonlinearity and nonlinear mobility appears since the initial damage. And uni-direction for this research applies the theory to have been confined to. On this study, we are going to get basically fiber properties and matrix than carbon composite properties for simulating according stacking method by GENOA-MCQ. It is help to simulate easily composite material. Also Calculate the matrix nonlinear for simulating non-linear.

• 한국자동차공학회논문집
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• 제11권6호
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• pp.197-204
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• 2003

This paper develops a computer model for estimating the handling of a cabover type large-sized truck. The truck is composed of front and rear suspension systems, a frame, a cab, and ten tires. The computer model is developed using ADAMS. A shock absorber, a rubber bush, and a leaf spring aunt a lot on the dynamic characteristic of the vehicle. Their stiffness and damping coefficient are measured and used as input data of the computer model. Leaf springs in the front and rear suspension systems are modeled by dividing them three links and joining them with joints. To improve the reliability of the developed computer model, the frame is considered as a flexible body. Thus, the frame is modeled by finite elements using MSC/PATRAN. A mode analysis is performed with the frame model using MSC/NASTRAN in order to link the frame model to the computer model. To verify the reliability of the developed computer model, a double lane change test is performed with an actual vehicle. In the double lane change, lateral acceleration, yaw rate, and roll angle are measured. Those test results are compared with the simulation results.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2005년도 춘계학술대회논문집
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• pp.813-820
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• 2005

In this study, finite element modeling and structural vibration analyses of a gyrocopter have been conducted considering dynamic hub-loads due to rotating blades. For this research, 3D CATIA models for most mechanical parts are exactly prepared and assembled into the final aircraft configuration. Then the dynamic finite element model including several non-structural parts are constructed based on the exact 3D CAD data. Computational structural dynamics technique based on finite element method is applied using both MSC/NASTRAN and developed in-house code which can largely reduce the pre and postprocessing time of general transient dynamic analyses. Modal based transient and frequency response analyses are used to efficiently investigate vibration characteristics. The results include natural frequency comparison for different fuel and pilot conditions, fundamental natural mode shapes, frequency responses and transient acceleration responses of the present gyrocopter model.