• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2009년 춘계학술대회논문집
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• pp.252-268
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• 2009

In the present study, a grid deformation technique has been incorporated into the unsteady compressible and incompressible viscous flow solvers on unstructured hybrid meshes. An algebraic method based on the basis decomposition of normal edge vector was used for the deformation of viscous elements, and a ball-vertex spring analogy was adopted for inviscid elements among several spring analogy methods due to its robustness. The present method was validated by comparing the results obtained from the grid deformation and the rigid motion of entire grids. Fish swimming motion of an NACA0012 airfoil and flapping wing motion of a generic fighter were simulated to demonstrate the robustness of the present grid deformation technique.

• 한국전산유체공학회지
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• 제9권1호
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• pp.48-56
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• 2004

The numerical simulations with unstructured mesh by cell-centered and vertex-centered approaches were peformed for the quadrilateral and triangular meshes. For 2-D inviscid supersonic vortex flow, the simulation results and the analytic solution were compared and the accuracy was assessed. The calculation efficiency was measured by the parameter defined by the consumed CPU time multiplied by absolute error As a results, equilateral triangular mesh yielded the best accuracy and efficiency among the tested meshes. Cell-centered approach gives a little better efficiency than vertex - centered approach.

• 한국전산유체공학회지
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• 제14권3호
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• pp.33-48
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• 2009

In the present study, a fast grid deformation technique has been incorporated into the unsteady compressible and incompressible viscous flow solvers on unstructured hybrid meshes. An algebraic method based on the basis decomposition of normal edge vector was used for the deformation of viscous elements, and a ball-vertex spring analogy was adopted for inviscid elements among several spring analogy methods due to its robustness. The present method was validated by comparing the results obtained from the grid deformation and the rigid motion of entire grids. Fish swimming motion of an NACA0012 airfoil and flapping wing motion of a generic fighter were also simulated to demonstrate the robustness of the present grid deformation technique.

• 자원환경지질
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• 제57권2호
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• pp.253-261
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• 2024

감람석은 강한 고유 탄성 이방성을 가진 상부 맨틀의 주요 광물이기 때문에 맨틀에서 발생하는 대부분의 지진파 비등방성은 감람석의 격자선호방향에서 직접적으로 기인한다. 그러나 압쇄암의 미구조가 지진파 비등방성에 미치는 영향에 대한 이해는 아직 잘 알려져 있지 않으며, 국내의 압쇄암화된 페리도타이트 암괴에서 직접적으로 추론한 지진파 비등방성 연구는 전무하다. 따라서 본 연구에서는 맨틀 전단대 내의 감람석의 변형 미구조와 격자선호방향을 소개하고, 이들의 변형 정도(원압쇄암, 압쇄암, 초압쇄암)와 격자선호방향 결과에 따른 지진파 비등방성의 특성을 계산하고 이들의 상관관계를 파악해보았다. 그 결과, 초압쇄암의 감람석 격자선호방향에서 기인한 지진파 비등방성은 가장 약하게 나타났고, 원압쇄암의 감람석 격자선호방향에서 기인한 지진파 비등방성은 가장 강하게 나타났다. 이러한 결과는 감람석의 격자선호방향의 패턴과는 관계없이 격자선호방향의 배열 강도(J-index)가 감소함에 따라 지진파 비등방성이 점차 감소하는 것으로 나타났다. 또한, 모든 샘플에서 공통적으로 빠른 S파의 편파방향이 선구조와 아평행하게 배열하는 것을 보여 주었다. 따라서 유구 페리도타이트 내 감람석에서 기인한 지진파 비등방성은 격자선호방향의 타입보다 배열 강도에 의해 지배된다고 설명할 수 있다. 이러한 서로 대조되는 지진파 비등방성의 특성을 잘 고려하면, 경기육괴 유구 지역의 맨틀의 내부 구조와 지진파 자료를 비교하고 해석하는데 도움을 줄 수 있을 것으로 기대한다.

• 전자통신동향분석
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• 제2권4호
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• pp.20-33
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• 1987

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2012년도 춘계학술대회 논문집
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• pp.568-569
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• 2012

• 한국자기학회:학술대회 개요집
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• 한국자기학회 2005년도 하계학술연구발표회 논문개요집
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• pp.180-181
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• 2005

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2005년도 춘계학술대회 논문집
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• pp.844-847
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• 2005

A seamless analysis of complex geometry is one of greatly interesting topic. However, there are still gaps between the industrial applications and fundamental academic studies owing to time consuming modeling process. To resolve this problem, an auto mesh generation program based on grid-based approach has been developed for IT-product in the present study. At first, base mesh and skin mesh are generated using the information of entities which extracted from IGES file. Secondly the provisional core mesh with rugged boundary geometry is constructed by superimposing the skin mesh as well as the base mesh generated from the CAD model. Finally, the positions of boundary nodes are adjusted to make a qualified mesh by adapting node modification and smoothing techniques. Also, for the sake of verification of mesh quality, the hexahedral auto mesh constructed by the program is compared with the corresponding tetrahedral free mesh and hexahedral mapped mesh through static finite element analyses. Thereby, it is anticipated that the grid-based approach can be used as a promising pre-processor for integrity evaluation of various IT-products.

• 한국전산유체공학회지
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• 제18권3호
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• pp.26-33
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• 2013

In the present study, unsteady flow simulations of a variable geometry nozzle were conducted using a two-dimensional flow solver based on hybrid unstructured meshes. The variable geometry nozzle is used to achieve efficient performances of aircraft engines at various operating conditions. To describe the motion of the variable geometry nozzle, an algebraic method based on the basis decomposition of normal edge vector was used for the deformation of viscous elements. A ball-vertex spring analogy was used for inviscid elements. The aerodynamic data were obtained for a range of nozzle pressure ratios, and the validations were made by comparing the present results with available experimental data. The unsteady nozzle flows were simulated with an oscillating diverging section and a converging-diverging section. It was found that the nozzle performances are influenced by the nozzle exit flow characteristics, mass flow rate, as well as unsteady effects. These unsteady effects are shown to behave differently depending on the frequency of the nozzle motion.

• 대한조선학회논문집
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• 제31권4호
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• pp.58-65
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• 1994

계산격자크기의 변화에 따른 해의 특성을 이해하는 것은 중요하며, 특히 벽함수를 사용하지 않는 난류모형을 사용할 때 더욱 그러하다. 본 논문에서는 배주위의 3차원 난류유동장에 대한 수치해의 격자의존성에 대한 수치계산적인 조사를 수행한다. 본 연구에서는 수정된 sub-grid-scale 난류모형과 함께 유한체적법을 사용하며 복잡한 배의 기하학적 형상에 적합한 비직교의 곡선좌표계를 수치적으로 만들어 사용한다. 그리고 수학선형인 Wigley 선형과 Series 60($C_B=0.8$) 선형에 대하여 수치계산적인 연구를 수행하고, 수치해의 격자의존성을 보이기 위하여 여러가지 격자크기에 대한 계산결과들을 서로 비교하였으며 실험결과와도 비교해 보인다.