• 항공우주기술
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• 제5권2호
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• pp.60-66
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• 2006

본 논문은 MSC/Nastran superelement를 이용한 연성하중해석에 대한 연구이다. 위성개발시 발사체가 선정되면, 발사체와 위성체간의 연성하중해석이 실시된다. 연성하중해석 결과로부터 위성구조체의 주요 부위에서의 하중과 변위를 도출하고, 이로부터 현 설계의 안정성을 판단하게 된다. 지금까지의 연성하중해석은 MSC/Nastran의 DMAP 코드를 이용하여 수행이 되었다. DMAP 코드의 경우 코드가 매우 복잡하고, 길기 때문에 코드 분석 및 수정에 어려움이 많았다. 이를 해결하기 위해서 MSC/Nastran 2005의 superelement를 이용하여 연성하중해석을 수행하였다. 던저 위성체 유한요소모델을 MSC/Nastran 2005 superelement를 이용하여 Craig-Bampton 모델로 변환하고 이를 정확성을 검증하었다. Craig-Bampton 모델로 변환된 위성체 모델을 발사체 모델과 접속하여 연성하중해석을 수행하였고, 이의 정확성을 검증하였다.

• Structural Engineering and Mechanics
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• 제27권2호
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• pp.243-257
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• 2007

A numerically efficient superelement is proposed as a low degree of freedom model for dynamic analysis of rotating tapered beams. The element uses a combination of polynomials and trigonometric functions as shape functions in what is also called the Fourier-p approach. Only a single element is needed to obtain good modal frequency prediction with the analysis and assembly time being considerably less than for conventional elements. The superelement also allows an easy incorporation of polynomial variations of mass and stiffness properties typically used to model helicopter and wind turbine blades. Comparable results are obtained using one superelement with only 14 degrees of freedom compared to 50 conventional finite elements with cubic shape functions with a total of 100 degrees of freedom for a rotating cantilever beam. Excellent agreement is also shown with results from the published literature for uniform and tapered beams with cantilever and hinged boundary conditions. The element developed in this work can be used to model rotating beam substructures as a part of complete finite element model of helicopters and wind turbines.

• 대한기계학회논문집
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• 제12권3호
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• pp.450-456
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• 1988

본 연구에서는 자동차의 동력학적 해석을 위한 특별프로그램을 만들어서 범용 프로그램인 DADS와 효율성을 비교해 보고자 한다.

• Structural Engineering and Mechanics
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• 제48권3호
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• pp.309-331
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• 2013

An integrated superelement concept is proposed to improve the computational efficiency when analyzing structural responses during progressive collapses of large-scale structures, such as multi-storey reinforced concrete buildings. While the proposed methodology is straightforward and can be implemented into an existing finite element program with little effort, it is able to significantly reduce the computational cost without the loss of any critical information of the structural responses. Compared with the models without superelement, significant saving in computational cost and satisfactory prediction accuracy can be obtained with the proposed approach.

• 한국기계가공학회지
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• 제21권3호
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• pp.86-91
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• 2022

The mechanical structures mounted on vehicles or aircrafts are subject to random accelerations, such as earthquakes, at the base, and their responses have been calculated through spectrum analysis. However, this method poses a challenge during the synthesis of the responses owing to the loss of the vibration phase. It is necessary to evaluate the time history results to obtain the exact responses; therefore, an efficient technique is proposed to solve this issue. The present technique involves constructing a superelement using the sub-structuring method and finding solutions for this superelement. The finite element model (FEM) was substituted by a superelement, which was simplified into one element with selected nodes. Comparing the numerical results of the superelement with the time history responses for the original finite element model, the two solutions agree well despite the fact that the computation time of the proposed technique has been greatly shortened.

• 한국위성정보통신학회논문지
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• 제6권2호
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• pp.46-50
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• 2011

인공위성에 대한 구조해석을 수행하기 위해서는 인공위성의 모든 기계적 특성이 반영된 유한요소모델을 필요로 한다. 인공위성의 개발특성상 여러 부품들은 서로 다른 회사에서 제작이 되며, 해당 유한요소모델의 제공이 불가능한 경우가 종종 발생하게 된다. 이러한 경우에 초요소 기법을 이용하면 쉽게 해결할 수 있다. 현재 개발중인 위성의 경우, 안테나 업체에서 안테나 기동시 발생하는 미소진동의 양을 계산하고자 인공위성 전체의 유한요소모델을 필요로 하였다. 이 때, 초요소 기법을 이용하여 축약된 모델을 제공할 수 있었다. 초요소기법은 Craig-Bampton 방법을 이용하여 유한요소모델을 동적축약하는 기법이며 본 논문에서는 인공위성 유한요소모델에 이를 적용하였다. 동적축약이 잘 이루어졌는지를 확인하기 위하여 전체 유한요소모델과, 축약모델의 모드해석 결과와 주파수 응답해석 결과를 비교하였으며, 두 결과가 매우 잘 맞는다는 것을 확인할 수 있었다. 이로부터 본 해석 방법의 유용성을 확인할 수 있었다.

• Structural Engineering and Mechanics
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• 제61권6호
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• pp.807-816
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• 2017

In this paper, we introduce an efficient new model reduction method, named the automated static condensation method, which is developed for the local analysis of large finite element models. The algebraic multilevel substructuring procedure is modified appropriately, and then applied to the original static condensation method. The retained substructure, which is the local finite element model to be analyzed, is defined, and then the remaining part of the global model is automatically partitioned into many omitted substructures in an algebraic perspective. For an efficient condensation procedure, a substructural tree diagram and substructural sets are established. Using these, the omitted substructures are sequentially condensed into the retained substructure to construct the reduced model. Using several large practical engineering problems, the performance of the proposed method is demonstrated in terms of its solution accuracy and computational efficiency, compared to the original static condensation method and the superelement technique.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 춘계학술대회논문집B
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• pp.341-348
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• 2001

In this study, a method is presented to find out a relationship between modes of a substructure and those of the system structure. Superelement analysis is performed for a full vehicle system, where the bus is partitioned by six parts. In this study, Modal Assurance Criteria(MAC) which is to represent the correlation between two mode shapes is used to investigate the contribution factor of each substructure for the full system. The proposed participation factor can be used for design of substructures to meet the design target of the total structural system.

• 한국CDE학회논문집
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• 제8권2호
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• pp.109-114
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• 2003

In order to develop the reduced tire modal model for analyzing a full tire model, the Craig-Bampton method is utilized in this paper. When the tire contacts the road, the Abaqus solver extracts the condensed stiffness, coupled mass and mode shape matrix about the node, which contacts the road. The Abaqus full tire model is reduced using the substructure method utilizing Craig-Bampton algorithm. Then, the extracted matrices are interfaced with the superelement, which is fed to the Nastran reduction algorithm. Eventually, the reduced tire model is verified from experiment and various reduction parameters (i.e. modal number, reduction point, etc.) are studied for the effectiveness of the proposed paper.

• 한국원자력학회:학술대회논문집
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• 한국원자력학회 2003년도 추계학술발표대회 요약집
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• pp.54.1-54.1
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• 2003