• 한국전산구조공학회논문집
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• 제23권6호
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• pp.659-665
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• 2010

The finite element method(FEM) is proven to be an effective approximate method of structural analysis if proper element types and meshes are chosen, and recently, the method is often applied to solve complex dynamic and nonlinear problems. A properly chosen element type and mesh yields reliable results for dynamic finite element structural analysis. However, dynamic behavior of a structure may include unpredictably large strains in some parts of the structure, and using the initial mesh throughout the duration of a dynamic analysis may include some elements to go through strains beyond the elements' reliable limits. Thus, the finite element mesh for a dynamic analysis must be dynamically adaptive, and considering the rapid process of analysis in real time, the dynamically adaptive finite element mesh generating schemes must be computationally efficient. In this paper, a computationally efficient dynamically adaptive finite element mesh generation scheme for dynamic analyses of structures is described. The concept of representative strain value is used for error estimates and the refinements of meshes use combinations of the h-method(node movement) and the r-method(element division). The shape coefficient for element mesh is used to correct overly distorted elements. The validity of the scheme is shown through a cantilever beam example under a concentrated load with varying values. The example shows reasonable accuracy and efficient computing time. Furthermore, the study shows the potential for the scheme's effective use in complex structural dynamic problems such as those under seismic or erratic wind loads.

• 한국정밀공학회지
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• 제16권12호
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• pp.99-108
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• 1999

A four-degree-of-freedom non-linear model with time varying mesh stiffness has been developed for the dynamic analysis of spur gear trains. The model includes a spur gear pair, two shafts, two inertias representing load and prime mover. In the model, developed several factors such as time varying mesh stiffness and damping, separation of teeth, teeth collision, various gear errors and profile modifications have been considered. Two computer programs are developed to calculate stiffness of a gear pair and transmission error and the dynamic analysis of modeled system using time integration method. Dynamic tooth and mesh forces, dynamic factors are calculated. Numerical examples have been given, which shows the time varying mesh stiffness ha a significant effect upon the dynamic tooth force and torsional vibrations.

• Journal of Computational Design and Engineering
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• 제1권2호
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• pp.96-102
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• 2014

In the field of design and manufacturing, there are many problems with managing dynamic states of three-dimensional (3D) objects. In order to solve these problems, the four-dimensional (4D) mesh model and its modeling system have been proposed. The 4D mesh model is defined as a 4D object model that is bounded by tetrahedral cells, and can represent spatio-temporal changes of a 3D object continuously. The 4D mesh model helps to solve dynamic problems of 3D models as geometric problems. However, the construction of the 4D mesh model is limited on the time-series 3D voxel data based method. This method is memory-hogging and requires much computing time. In this research, we propose a new method of constructing the 4D mesh model that derives from the 3D mesh model with continuous rigid body movement. This method is realized by making a swept shape of a 3D mesh model in the fourth dimension and its tetrahedralization. Here, the rigid body movement is a screwed movement, which is a combination of translational and rotational movement.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2006년도 춘계학술대회논문집
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• pp.224-231
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• 2006

A six-degree-of-freedom dynamic model with time-varying mesh stiffness/damping and friction has been developed for the dynamic analysis of a gear driving system. This model includes a spur gear pair, bearing, friction and prime mover. Using Newton???s method, equations of motion for the gear driving system were derived. Two computer programs are developed to calculate mesh stiffness, transmission error and friction force and analyze the dynamics of the modeled system using a time integration method. The influences of mesh stiffness/damping, bearing, and friction affecting the system were investigated by performing eigenvalue analysis and time response analysis. It is found that the reduction of the maximum peak magnitude by friction is decided according to designing the positions of pitch point and maximum peak in the responses.

• 대한전기학회논문지:전기기기및에너지변환시스템부문B
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• 제50권2호
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• pp.53-58
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• 2001

This paper describes a moving mesh technique for dynamic characteristics analysis of permanent magnet linear synchronous motor with the secondary aluminium sheet. The moving mesh technique applied to the linear induction motor can be used to analyze the linear synchronous motor with the rectangular permanent magnet. But in case of the permanent magnet with taper, the shape of the permanent magnet is presented. The time-stepped finite element method is used for the dynamic characteristics simulation of the permanent magnet linear synchronous motor, The results of application example(hysteresis current controlled inverter fed control) such as thrust, current and flux plots are shown.

• 방송공학회논문지
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• 제28권3호
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• pp.314-328
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• 2023

본 논문에서는 동적 메쉬 부/복호화 시 스케일러빌리티 기능을 지원하기 위해 SHVC의 계층적 부호화 방식을 기반으로 텍스처 맵을 압축하는 방법을 제안한다. 제안하는 방법은 고해상도 텍스처 맵을 다운샘플링하여 다해상도의 텍스처 맵을 생성하고 이를 SHVC로 부호화함으로써 효과적으로 다해상도 텍스처 맵들의 중복성을 제거한다. 동적 메쉬 복호화기에서는 수신기 성능, 네트워크 환경 등에 따라 적합한 해상도의 텍스처 맵을 복호화하여 메쉬 데이터의 스케일러빌리티를 지원할 수 있도록 한다. 제안하는 방법의 성능을 검증하기 위해 V-DMC (Video-based Dynamic Mesh Coding) 참조 소프트웨어인 TMMv1.0에 제안하는 방법을 적용하고 본 논문에서 제안하는 스케일러블 부/복호화기와 TMMv1.0 기반의 시뮬캐스트 방식의 성능을 비교하였다. 제안하는 방법은 시뮬캐스트 방법 대비 AI, LD 환경에서 Luma BD-rate (Luma PSNR)가 각각 평균 -7.7%, -5.7%의 향상된 결과를 얻어 제안하는 방법을 통해 효과적으로 동적 메쉬 데이터의 텍스처 맵 스케일러빌리티 지원이 가능함을 확인하였다.

• 한국지반공학회:학술대회논문집
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• 한국지반공학회 2009년도 세계 도시지반공학 심포지엄
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• pp.1441-1446
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• 2009

Numerical analysis is a powerful method in evaluating the soil-pile-structure interaction under the dynamic loading, and this approach has been applied to the practical area due to the development of computer technology. Finite Difference Method, one of the most popular numerical methods, is sensitive to the shape and the number of mesh. However, the trial and error approach is conducted to obtain the accurate results and the reasonable simulation time because of the lack of researches about mesh size and the number. In this study, FLAC 3D v3.1 program(FDM) is used to simulate the dynamic pile model tests, and the numerical results are compared with the 1G shaking table tests results. With the different size and shape of mesh, the responses of pile behavior and the simulation time are estimated, and the optimum mesh sizes in dynamic analysis of single pile is studied.

• 한국지반공학회논문집
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• 제22권4호
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• pp.5-10
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• 2006

반무한 영역을 유한영역에 사영한 다음 반무한지반의 비선형동적응답해석에 대한 특수한 유한 차분법을 제안하였다. 해석대상의 주요 부분은 동일 길이로 하고, 주변은 축소, 사영함으로서 무한영역을 유한영역으로 변환 후 차분하였다. 우선 반무한 지반의 선형모델의 응답으로서 계산값과 이론값의 결과를 비교하였다. 선형모델에 대한 제안법의 계산결과는 Lamb의 해석결과와 양호하게 일치했다. 또 간단한 모델에 의한 선형, 비선형해석도 소규모 mesh에 의한 응답결과와 대규모 mesh에 의한 응답결과는 일치하고 제안법의 유효성을 나타내었다.

• Structural Engineering and Mechanics
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• 제31권4호
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• pp.383-392
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• 2009

The static and dynamic analyses of simply supported beams are studied by using the U-transformation method and the finite difference method. When the beam is divided into the mesh of equal elements, the mesh may be treated as a periodic structure. After an equivalent cyclic periodic system is established, the difference governing equation for such an equivalent system can be uncoupled by applying the U-transformation. Therefore, a set of single-degree-of-freedom equations is formed. These equations can be used to obtain exact analytical solutions of the deflections, bending moments, buckling loads, natural frequencies and dynamic responses of the beam subjected to particular loads or excitations. When the number of elements approaches to infinity, the exact error expression and the exact convergence rates of the difference solutions are obtained. These exact results cannot be easily derived if other methods are used instead.

• 한국항공우주학회지
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• 제43권3호
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• pp.232-242
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• 2015

기동 성능과 스텔스 성능을 극대화시키기 위해 무미익 람다(lambda) 형상의 무인전투기에 대한 연구개발이 각 국에서 활발히 진행되고 있다. 이러한 형상의 비행체는 불안정한 동적 비행특성을 가질 가능성이 높으며, 이를 비행제어 시스템으로 제어하기 위해서는 보다 정확한 동안정 미계수 예측이 필수적이다. 본 연구에서는 풍동기법의 단점을 보완하고 순수 공기역학적 동안정 미계수를 예측하기 위해 전산유체역학의 Dynamic Mesh 기법을 적용하여 강제진동법을 모사하였고, 해석결과를 기존에 확보한 시험결과와 비교하여 검증하였다. 해석결과는 종축 동안정 미계수에 국한하였으며, 무미익 람다 형상의 기준 받음 각, 진동주파수, 진동폭 등의 변화에 따른 동안정 미계수 변화 경향성을 파악하였다. 전산해석 결과는 풍동시험 데이터와 유사한 경향성을 보였으며, 제시된 연구기법을 통해 항공기 동안정 미계수를 효율적으로 구할 수 있음을 확인하였다.