• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2013.04a
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• pp.180-185
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• 2013

A new formulation of the MNDIF method is introduced to extract highly accurate natural frequencies of concave plates with arbitrary shape. Originally, the MNDIF method cannot yield accurate natural frequencies for concave plates. To overcome this weak point, a new approach of dividing a concave plate into two convex domains is proposed and the validity and accuracy is shown in a verification example.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 1994.10a
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• pp.173-180
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• 1994

본 논문에서는 임의 형상의 블록 다각형 박막 고유 진동해석을 위해 파 형태의 해석해를 사용하는 새로운 기법을 제시하였다. 파 형태의 해석해를 임의 형상의 박막에 사용하는 데 있어 나타날 수 있는 시도해의 종속적인 문제점을 지적하고, 이를 극복하는 방안을 제시하였다. 여러 수치 예제를 통해 본 기법의 유용성과 타당성을 보였고, 특히 이 기법은 특정 주파수 대역에서 고유 진동수를 찾고자 할 때, 매우 효율적임을 알 수 있다. 본 논문은 기초 연구로서 제한된 모든 변이 고정된 블록 다각형 형상의 박막의 고유 진동 해석만 수행하였지만, 이 기법을 확장, 발전시켜 나가면, 어떠한 형상이나 경계조건을 갖는 박막뿐만 아니라 평판의 진동 해석에도 적용할 수 있으리라 기대하며, 이를 위한 연구가 진행중이다.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2011.04a
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• pp.329-330
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• 2011

• Transactions of the Korean Society for Noise and Vibration Engineering
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• v.26 no.5
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• pp.602-608
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• 2016

The paper proposes a practical meshless method for the free vibration analysis of clamped plates having arbitrary shapes by extending the non-dimensional dynamic influence function (NDIF) method, which was developed by the author in 1999. In the proposed method, the domain and boundary of the plate of interest are discretized using only nodes without elements unlike FEM and the system matrices are obtained by making domain nodes and boundary nodes satisfy the governing differential equation and boundary conditions, respectively. However, since the above system matrices are not square ones, the problem of free vibrations of clamped plates is not reduced to an algebraic eigenvalue problem. An additional theoretical treatment is considered to produce an algebraic eigenvalue problem. It is revealed from case studies that the proposed method is valid and accurate.

• Journal of the Society of Naval Architects of Korea
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• v.32 no.3
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• pp.116-125
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• 1995

In ship and of offshore structures, there exist many local panels of various shapes having many kinds of attachments reducible to damped spring-mass systems. For the vibration analysis of panels, analytical methods such as Rayleight-Ritz method or the assumed mode method can be efficiently applied. There have been many studies on the vibration analysis of rectangular panels using the analytical methods but relatively few for arbitrary shape panels. An efficient formulation based on the assumed mode method is presented for the vibration analysis of an arbitrary quadrangular plate having concentrated masses, supporting springs such as pillars and spring-mass systems. In the formulation, the natural coordinate system is used for the efficient treatment of an arbitrary quadrangular shape. Through some numerical calculations, accuracy and efficiency of the presented method are shown.

• Proceedings of the KSME Conference
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• 2005.11a
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• pp.184.2-184.2
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• 2005

• Proceedings of the KIEE Conference
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• 2005.04a
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• pp.9-11
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• 2005

영구자석형 선형발전기의 설계에 있어서 주로 고려되어야 할 사항은 영구자석, 철심형 치 및 코일의 형상 설계이다. 또한 영구자석과 철심형 치의 상호 작용에 의한 디텐트력은 기기의 안정적인 성능을 위해 저감되어야 한다. 본 논문에서는 1kW급 왕복 구동 평판형 선형 발전기의 영구자석과 치의 구조에 따른 디텐트력과 역기전력의 변화를 유한요소법을 이용하여 해석하였고, 디텐트력의 저감을 위해 다양한 구조의 영구자석과 치 형상이 적용되었다. 기기 구조의 변화는 역기전력에도 영향을 끼치므로 적용된 설계안 중 역기전력의 손실을 최소화할 수 있도록 설계안의 적절한 선택이 필요하다.

• Transactions of the Korean Society for Noise and Vibration Engineering
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• v.25 no.11
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• pp.779-786
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• 2015

The Kansa method, which is used for various free vibration problems of arbitrarily shaped plates including membranes, discretizes the domain of a plate using only nodes without elements unlike FEM. The method requires a small amount of computation relative to FEM thanks to this discretization scheme but has limit in the accuracy of its solution. This paper reveals the reason of the limit and, to overcome the limit, proposes the practical method of calculating the singularity of a system matrix and extracting accurate natural frequencies. Case studies for a rectangular plate and an arbitrarily shaped plate validate the proposed method.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.27 no.8
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• pp.1331-1337
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• 2003

Linearized equations of motion for the vibration analysis of rotating cantilever plates with arbitrary orientation angle are derived in the present work. Two in-plane stretch variables are introduced to be approximated. The use of the two in-plane stretch variables enables one to derive the equations of motion which include proper motion-induced stiffness variation terms. The equations of motion are transformed into dimensionless forms in which dimensionless parameters are identified. The effects of the dimensionless parameters on the modal characteristics of rotating cantilever plates are investigated through numerical study. The natural frequency loci veering along with the associated mode shape variations, which occur while the rotating speed increases, are also presented and discussed.

• Journal of the Korea institute for structural maintenance and inspection
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• v.8 no.2
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• pp.147-158
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• 2004

For stiffened plates composed of composite materials, many researchers have used a finite element method which connected isoparametric plate elements and beam elements. However, the finite element method is difficult to reflect local behavior of stiffener because beam elements are transferred stiffness for nodal point of plate elements, especially the application is limited in case of laminated composite structures. In this paper, for analysis of laminated composite stiffened plates, 3D shell elements for stiffener and plate are employed. Reissner-Mindlin's first order shear deformation theory is considered in this study. But when thickness will be thin, isoparamatric plate bending element based on the theory of Reissner-Mindlin is generated by transverse shear locking. To eliminate the shear locking and virtual zero energy mode, the substitute shear strain field is used. A deflection distribution is investigated for simple supported rectangular and skew stiffened laminated composite plates with arbitrary orientation stiffener as not only variation of slenderness and aspect ratio of the plate but also variation of skew angle of skew stiffened plates.