• 소성∙가공
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• 제21권8호
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• pp.479-484
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• 2012

The objective of this study is to compensate the elastic recovery in the flexible forming process using the predictive models. The target shape was limited to two-dimensional shape having only one curvature radius in the longitudinal-direction. In order to predict the shape error the regression and neural network models were established based on the finite element (FE) simulations. A series of simulations were conducted considering input variables such as the elastic pad thickness, the thickness of plate, and the objective curvature radius. Then, at sampling points in the longitudinal-direction, the shape errors between formed and objective shapes could be calculated from the FE simulations as an output variable. These shape errors were expressed to a representative error value by the root mean square error (RMSE). To obtain the correct objective shape the die shape was adjusted by the closed-loop using the neural network model since the neural network model shows a higher capability of estimating the shape error than the regression model. Finally the experimental result shows that the formed shape almost agreed with the objective shape.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2009년 춘계학술대회논문집
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• pp.57-65
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• 2009

An efficient and high-fidelity design approach for wing-body shape optimization is presented. Depending on the size of design space and the number of design of variable, aerodynamic shape optimization process is carried out via different optimization strategies at each design stage. In the first stage, global optimization techniques are applied to planform design with a few geometric design variables. In the second stage, local optimization techniques are used for wing surface design with a lot of design variables to maintain a sufficient design space with a high DOF (Degree of Freedom) geometric change. For global optimization, Kriging method in conjunction with Genetic Algorithm (GA) is used. Asearching algorithm of EI (Expected Improvement) points is introduced to enhance the quality of global optimization for the wing-planform design. For local optimization, a discrete adjoint method is adopted. By the successive combination of global and local optimization techniques, drag minimization is performed for a multi-body aircraft configuration while maintaining the baseline lift and the wing weight at the same time. Through the design process, performances of the test models are remarkably improved in comparison with the single stage design approach. The performance of the proposed design framework including wing planform design variables can be efficiently evaluated by the drag decomposition method, which can examine the improvement of various drag components, such as induced drag, wave drag, viscous drag and profile drag.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2001년도 춘계 학술대회논문집
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• pp.72-77
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• 2001

The computational efficiency of an shape optimization procedure is highly dependent upon the proper selection of shape representation methods and design variables. In this study, shape functions, Bezier and NURBS(non-uniform rational B-splines) curves are selected as configuration generation methods and their efficiencies on the nose shape design of high-speed air vehicles, are compared. The effects of the number of control points, weighting factors and the optimization methods when utilizing the NURBS curves, are investigated. By implementing Bezier and NURBS curves, shapes having lower drag than the optimization case utilizing the shape functions, were obtained, hence it was demonstrated that these curves have better capability in representing the configuration. Efforts will be given to improve the convergence behavior when utilizing the NURBS, hence to reduce the number of Navier-Stokes analysis calculations.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2000년도 추계학술대회 논문집
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• pp.616-619
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• 2000

The optimum design of a structure requires to determine economical member size and shape of a structure which satisfies the design conditions and functions. In this study, it is attempted to minimize a dead weight of the bogie frame. Therefore, shape optimization is performed for a bolster rib at first and then size optimization for the thickness of top and bottom plate. For the efficient reduction of a weight of a bogie frame, various ellipses centered at a centroid of a bolster rib are made and tried. For the shape optimization, a major axis and an eccentricity of an ellipse are chosen as design variables. From the numerical results of shape and size optimization of a bogie frame, it is known that the weight can be reduced up to 12.476 Y4717.21 kg) with displacement and stress constraints.

• 한국자동차공학회논문집
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• 제25권2호
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• pp.242-249
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• 2017

In this study, the relationship between the shape of a passenger airbag and the possibility of injury is analyzed using the Taguchi method. The optimal shape combination is proposed for a design guideline that can reduce the possibility of injury to the dummy. The airbag FE model for analysis is obtained using a CAD system that can change the shape through several independent variables. The widths of the left / right, top / bottom, and back / forth direction of the airbag shape are set as the design factors, and the effect of the combination injury probability according to the shape is analyzed. The minimum geometric combinations are obtained using the orthogonal array method. The signal to noise ratio is calculated and the optimal shape combination is obtained through sensitivity analysis. The obtained optimal shape combination is compared with the possibility of injury of the initial airbag shape to confirm improved airbag performance.

• 응용통계연구
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• 제37권1호
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• pp.73-86
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• 2024

평가지표와 같은 수치형 자료의 경우 수치 형태보다 엑셀(Excel)의 방사형 차트 형태로 나타내 시각적으로 표현하면 정보 전달에 더욱 효과적일 것이다. 그러나 개체가 많은 경우 시각적으로 판별하거나 분류하는 것이 쉽지 않다. 이럴 경우 각 개체에 대해 방사형 차트를 이용하여 형상화 시킨 후, 형상의 정보를 대표할 수 있는 형상점을 찾고 형상좌표로 변환해 형상분석을 적용하여 분류 및 판별하는 방법을 알아보고자 한다. 형상분석을 이용하기 위해 주로 분석자의 주관으로 형상점을 얻고 임의의 좌표공간을 생성시켜 좌표를 얻곤 했다. 방사형 차트는 해당 개체의 특징을 나타내는 변수의 개수만큼 형상점이 생기게 되고 이를 선으로 이은 것은 하나의 형상으로 여겨진다. 따라서 중심을 원점으로 두고 2차원 공간으로 정의를 내린 후, X축과 각 특징을 나타내는 축이 이루는 각에 대해 삼각함수를 적용해 형상좌표를 추출해낸다. 변수의 개수가 많아 형상의 모양이 복잡해질 경우 방사형 차트를 이용해 시각화하더라도 쉽게 파악하기 어렵다. 독립성을 보장할 수 없는 변수들에 대해 주성분 분석(PCA)을 실시하여 시각적으로 효과적인 형상을 만든다. PCA를 실시하기 전과 후의 형상에 대해 전통적 판별분석, 서포트벡터머신(support vector machine; SVM), 인공신경망(artificial neural network; ANN)의 기법을 적용시켜 분류표와 분류율을 확인한다. 또한 GPA (generalized procrustes analysis) 적합좌표, 북스테인좌표 2가지 좌표에 대한 판별의 차이를 비교한다. 북스테인좌표의 경우 기저 형상점을 중심으로 형상의 위치와 회전, 척도를 변환한 좌표로써, 분류율에 대해 GPA 형상좌표보다 더 높은 결과를 보이고 있다. 북스테인좌표의 경우 여러 군집 간의 형상을 비교하는데 유용하게 활용된다.

• 응용통계연구
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• 제25권3호
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• pp.521-529
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• 2012

Simple canonical correlation biplot is a graphical method to investigate two sets of variables and observations in simple canonical correlation analysis. If we consider the set of covariate variables that linearly affects two sets of variables, we can apply the partial canonical correlation biplot in partial canonical correlation analysis that removes the linear effect of the set of covariate variables on two sets of variables. On the other hand, we consider the set of covariate variables that linearly affect one set of variables but not the other. In this case, if we apply the simple or partial canonical correlation biplot, we cannot clearly interpret other two sets of variables. Therefore, in this study, we will apply the semi-partial canonical correlation analysis of Timm (2002) and remove the linear effect of the set of covariate variables on one set of variables but not the other. And we suggest the semi-partial canonical correlation biplot for interpreting the semi-partial canonical correlation analysis. In addition, we will compare shapes and shape the variabilities of the simple, partial and semi-partial canonical correlation biplots using a procrustes analysis.

• 인지과학
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• 제29권4호
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• pp.193-220
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• 2018

시각 단어 재인에 영향을 미치는 변인으로는 단어 빈도, 단어 길이, 이웃단어, 단어 형태 등이 밝혀진 바 있다. 단어 형태 변인은 한글이 영어와는 글자 체계가 다르기 때문에 형태 정보가 단어 처리에 다른 방식으로 영향을 미칠 수 있다. 본 연구는 게스탈트의 연속성 원리를 한글에 적용하여 한글 단어의 처리 단위를 알아보고, 음절 형태가 한글 단어 재인에 영향을 미치는지 검증하고자 하였다. 실험 1에서는 3음절 단어를 사용하여 음절 유형(평소 읽기방향이 연속성 원리에 부합하는 '가로집자'형(예: "가"), 부합하지 않는 '세로집자'형(예: "고")과 글자 제시 방향(가로, 세로)을 조작하였다. 어휘 판단 시간의 분석 결과, 제시 방향에 상관없이 '가로집자'형의 처리 속도가 '세로집자'형보다 빨랐다. 실험 2에서는 차폐 점화를 사용하여 음절유형('가로집자'와 '세로집자'형) 및 점화 자극과 목표 자극의 시각적 관계(동일, 유사, 상이)를 조작하였다. 점화자극과 목표자극의 음절집자 형태에 따라서 수행에 차이가 있었으며 이는 음절 형태가 단어 재인에 미친다는 것을 시사한다.

• 한국전산유체공학회지
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• 제4권1호
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• pp.34-40
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• 1999

Drag reduction on vehicles are the main concern for the body shape designers in order to lower the fuel consumption rate and to aid the driving stability. The drag of bluff bodies like transportation vehicles is mostly pressure drag due to the flow separation, which can be minimized by controlling the location and size of the separation bubble. In the present study, the TURBO-3D code is incorporated with optimal algorithm based on analytical approximation method to obtain an optimal afterbody shape of the MIRA Model corresponding to the lowest drag coefficient. For this purpose three mutually independent afterbody angles are chosen as design variables, while the drag coefficient is chosen as an objective function. It is demonstrated in the present study that an optimal body shape having the lowest drag coefficient which is about 6% lower than that of the original shape has been successfully obtained within number of iterations of tile optimal design loop.

• 대한기계학회논문집B
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• 제31권8호
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• pp.711-717
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• 2007

Shape optimization of a staggered herringbone groove micromixer using three-dimensional Navier-Stokes analysis has been carried using Kriging model. The analysis of the degree of mixing is performed by the calculation of spatial data statistics. The calculation of the variance of the mass fraction at various nodes on a plane in the channel is used to quantify mixing. A numerical optimization technique with Kriging model is applied to optimize the shape of the grooves on a single wall of the channel. Three design variables, namely, the ratio of groove width to groove pitch, the ratio of the groove depth to channel height ratio and the angle of the groove, are selected for optimization. A mixing index is used as the objective function. The results of the optimization show that the mixing is very sensitive to the shape of the groove which can be used in controlling mixing in microdevices.