• 한국전산구조공학회논문집
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• 제20권5호
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• pp.533-541
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• 2007

계층적 p-세분화를 위해 Zienkiewicz-Zhu 오차평가법이 약간 수정되었으며, 이 방법의 유효성을 보이기 위해 휨을 받는 개구부를 갖는 Reinssner-Mindlin $C^{\circ}$-평판에 적용하였다. 유한요소해석상의 적응적 체눈을 결정하는 단계는 초수렴 팻취 복구기법에 기초를 둔 사후오차평가자와 연계된 p-세분화에 의해 제안되었다. 요소내의 변위장을 정의하기 위해 적분형 르장드르 고차 형상함수가 사용되는 반면 복구응력을 보간하기 위해 파스칼의 삼각수에 기초를 둔 같은 차수의 고차다항식이 사용되는 이유로 수정 Z/Z 오차평가는 종래의 방법과 다소 차이를 보여준다. 가우스 적분점에서의 응력을 최적화하기 위해 필요한 다항식으로 표현되는 응력함수를 얻기 위해 최소제곱법이 사용되었다. 고정된 요소망에 거의 최적의 형상함수 차수의 분배를 찾기 위한 전략이 논의되었는데, 허용되는 정확도를 얻을 수 있을 때까지 각 요소마다 형상함수의 차수를 불균등하게 증가시키는 방법으로, 소위 최적의 선택적 p-분배를 자동으로 결정하도록 되어있다. 위의 사항들을 L-형 평판 해석에 적용한 결과, 적응적 p-체눈설계 단계가 진행됨에 따라 자유도의 증가에 따라 오차량은 급격히 감소되는 것을 알 수 있었고, 제안된 오차 지시자에 의한 적응적 p-체눈 세분화는 최적 p-분배 진행방향에 근접하는 것을 볼 수 있었다.

• The Korean Journal of Ceramics
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• 제6권3호
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• pp.236-239
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• 2000

Both the X-ray diffraction data of the normal direction in the sample orientation and the pole figure data of three reflections, (111), (200) and (220), were used to do the Rietveld refinement for the copper sheet prepared by a cold rolling process. The agreement between calculated and observed patterns was not satisfactory, which was attributed to the preferred orientation effect of the copper sheet. The Rietveld refinement for the copper sheet could be done successfully by applying the pole density of each reflection obtained from the corresponding inverse pole figure to the X-ray diffraction data of the normal direction. The R-weighted pattern, $R_{wp}$ was 12.99% and the goodness-of-fit indicator, S, was 3.68.

• 대한수학회논문집
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• 제15권1호
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• pp.59-69
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• 2000

For a permutation ${\mu}$ in S$\sub$b/, the limit algebra A${\mu}$ of the stationary system given by ${\mu}$ is isomorphic to a refinement limit algebra if and only if its exponent set E(${\mu}$) is the set {0}. In the current paper, we prove a sufficient condition under which E(${\mu}$)={0} when the order of ${\mu}$ is a power of p, where p is a prime number dividing b.

• 한국세라믹학회지
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• 제40권6호
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• pp.513-518
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• 2003

La/sub 2/3-x/Li/sub 3x/□/sub 1/3-2x/TiO₃ compounds with x=0.13 and 0.12 were prepared by slow cooling (x=0.13) and rapid quenching (x=0.12) into the liquid nitrogen after sintering at 1350℃ for 6 h. Their crystal structure has been determined by Rietveld refinement of both the powder neutron and X-ray diffraction data. From neutron diffraction data, we found that the main phase was not tetragonal (P4/mmm), but trigonal (R3cH). The refinement of neutron diffraction for the slow cooled samples were in a good agreement with a new model; a mixture of trigonal (R3cH, 45.7 wt％), tetragonal (p4/mmm, 37.0 wt％), and Li/sub 0.57/Ti/sub 0.86/O₂(pbnm, 17.2 wt%), but the quenched sample was found not to contain tetragonal (p4/mmm). X-ray diffraction data couldn't be well fitted because of the Poor scattering factor of lithium ions and the similar reflection patterns among trigonal (R3cH), tetragonal (p4/mmm), and cubic (Pm3m). We also knew that one transport bottlenecks is destroyed by one La vacancy in the case of trigonal (R3cH).

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 2006년도 정기 학술대회 논문집
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• pp.849-856
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• 2006

This paper is to examine the applicability of ordinary Kriging interpolation(OK) to the p-adaptivity of the finite element analysis that is based on variogram. In the p-refinement, the analytical domain has to be refined automatically to obtain an acceptable level of accuracy by increasing the p-level non-uniformly or selectively. In case of non-uniform p-distribution, the continuity between elements with different polynomial orders is achieved by assigning zero higher-order derivatives associated with the edge in common with the lower-order derivatives. It is demonstrated that the validity of the proposed approach by analyzing results for stress singularity problem.

• Structural Engineering and Mechanics
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• 제11권5호
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• pp.535-546
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• 2001

A new p-adaptive analysis scheme for hp-clouds method is presented. In the scheme, refined global equations are resolved into two parts, one of them being related to the newly appended dof's. The solution obtained in previous analysis step is reflected in the force vector. The size of the p-adaptive equation consisting of the newly appended dof's is much smaller than the original equation. Consequently, the computational cost is drastically decreased. Through numerical examples, the efficiency and efficacy of the method in comparison with the existing p-refinement scheme of the hp-clouds have been demonstrated.

• Structural Engineering and Mechanics
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• 제39권6호
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• pp.767-793
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• 2011

An efficient edge-based smoothed finite element method (ES-FEM) has been recently developed for solving solid mechanics problems. The ES-FEM uses triangular elements that can be generated easily for complicated domains. In this paper, the complexity study of the ES-FEM based on triangular elements is conducted in detail, which confirms the ES-FEM produces higher computational efficiency compared to the FEM. Therefore, the ES-FEM offers an excellent platform for adaptive analysis, and this paper presents an efficient adaptive procedure based on the ES-FEM. A smoothing domain based energy (SDE) error estimate is first devised making use of the features of the ES-FEM. The present error estimate differs from the conventional approaches and evaluates error based on smoothing domains used in the ES-FEM. A local refinement technique based on the Delaunay algorithm is then implemented to achieve high efficiency in the mesh refinement. In this refinement technique, each node is assigned a scaling factor to control the local nodal density, and refinement of the neighborhood of a node is accomplished simply by adjusting its scaling factor. Intensive numerical studies, including an actual engineering problem of an automobile part, show that the proposed adaptive procedure is effective and efficient in producing solutions of desired accuracy.

• International Journal of Aeronautical and Space Sciences
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• 제18권4호
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• pp.601-613
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• 2017

An adjoint-based error estimation and mesh adaptation study is conducted for two-dimensional viscous flows on unstructured hybrid meshes. The error in an integral output functional of interest is estimated by a dot product of the residual vector and adjoint variable vector. Regions for the mesh to be adapted are selected based on the amount of local error at each nodal point. Triangular cells in the adaptive regions are refined by regular refinement, and quadrangular cells near viscous walls are bisected accordingly. The present procedure is applied to single-element airfoils such as the RAE2822 at a transonic regime and a diamond-shaped airfoil at a supersonic regime. Then the 30P30N multi-element airfoil at a low subsonic regime with a high incidence angle (${\alpha}=21deg.$) is analyzed. The same level of prediction accuracy for lift and drag is achieved with much less mesh points than the uniform mesh refinement approach. The detailed procedure of the adjoint-based mesh refinement for the multi-element airfoil case show that the basic flow features around the airfoil should be resolved so that the adjoint method can accurately estimate an output error.

• 한국공간구조학회논문집
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• 제8권4호
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• pp.81-90
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• 2008

이 논문에서는 적분형 르장드르 다항식을 사용한 3차원 계층적 고체요소의 유한요소 정식화를 보여준다. 제안하는 육면체 고체요소는 절점, 변, 면, 그리고 내부모우드를 포함한은 4개의 서로 다른 모우드로 구성되어 있다. 영에너지 모우드와 일정변형률 조건을 확인하기 위해 고유치 시험과 조각시험이 수행되었다. 여기에 추가되어, 적응적 p-유한요소해석을 위해 유한요소해석으로부터 구한 후처리 응력값의 평활화에 기초를 둔 사후오차평가 기법이 연구된다. 자유도가 증가함에 따라 수렴속도측면에서 균등 p-분배와 불균등 p-분배에 의한 유한요소해의 차이점이 비교된다. 제안된 요소의 성능을 보이기 위해 간단한 캔틸레버보가 테스트되었다.

• 한국공간구조학회논문집
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• 제12권2호
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• pp.45-53
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• 2012

본 논문은 비정형의 정확한 형상 설계와 구조해석을 위해 넙스 기저함수를 기반으로 한 변수들로 생성된 평연의 등기하 해석법과 해석 결과에 대한 후처리 방법을 제시한다. 제어점, 매듭값, 차수들로 구성되는 변수들을 인터페이스 기법을 통해 변화시킴으로써 다양한 기하 형상을 구축할 수 있다. 등기하 해석에 사용되는 기저함수는 기하형상 구축에 사용되는 함수와 동일하여 형상의 정확한 설계와 해석이 가능하다. 등기하 해석을 위한 요소망 생성을 위해 h-p-k refinement 과정을 수행함으로써 기존 형상의 변형없이 요소망을 생성하여 구조해석을 수행하였다. 해석에 의한 결과값인 제어점의 변위에 대한 시각화를 위해 IGES 포맷과 넙스기반 3D 설계 프로그램 라이노와의 인터페이스 과정을 수행하여 최종 변형 형상 표현을 위한 후처리 방법을 제시한다.