• 한국유체기계학회 논문집
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• 제17권3호
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• pp.5-12
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• 2014

This paper presents a design optimization for meridional profile and blade angle ${\theta}$ of a centrifugal compressor with DOE (design of experiments) and RSM (response surface method). Control points of the $3^{rd}$ order Bezier curve are used for design parameters and specific overall efficiency is used as object function. The response surface function shows good agreement with the 3D computational results. Three different optimized designs are proposed and compared with reference design at design point and off-design point. Contours of relative Mach number, static entropy, and total pressure are analyzed for improvement of performance by optimization. Off-design performance analysis is conducted by total pressure and efficiency.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2003년도 추계학술대회논문집
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• pp.183-188
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• 2003

This study is to make the fundamentals of sound quality evaluation in regard of acoustical characteristics of passenger compartment. The deviation of frequency response function level within audible frequency is evaluated at receiving point in the research of room acoustics. In this study, frequency response function is the one between speaker and driver's ear positions. The positions of driver and audio speakers are optimized by analysis of acoustic mode of acoustic cavity. The main reflection planes are determined by analysis sound ray path diffused at optimized speaker positions. Finally, designer selects acoustical material by analysis of absorption effect of acoustical materials on the main reflection planes in order to avoid to distortion and fluctuation of frequency response function..

• 오토저널
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• 제15권1호
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• pp.81-88
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• 1993

A direct treatment of the min-max type objective function of the dynamic response optimization problem is proposed. Previously, the min-max type objective function was transformed to an artificial design variable and an additional point-wise state variable constraint function was imposed, which increased the complexity of the optimization problem. Especially, the design sensitivity analysis for the augmented Lagrangian functional with the suggested treatment is established by using the adjoint variable method and a computer program to implement the proposed algorithm is developed. The optimization result of the proposed treatment are obtained for three typical problems and compared with those of the previous treatment. It is concluded that the suggested treatment in much more efficient in the computational effort than the previous treatment with giving the similar optimal solutions.

• Composites Research
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• 제23권2호
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• pp.40-47
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• 2010

본 논문에서는 복합 반응면 기법을 제안하고 성능을 고찰하였다. 복합 반응면 기법은 MPP의 좌표를 기준으로 하여 근사모델을 반복 계산하는 기법이다. 성능을 검증하기 위해 비선형 함수와 복합재 적층판에 대하여 신뢰성 해석 기법을 적용하여 파괴확률, MPP(Most Probable failure Point), 신뢰도 지수를 계산하고 일반적인 반응면 기법의 결과와 비교하였다. 파괴확률은 비선형 한계상태식을 가정하고 임의의 파괴 기준을 정의하여 계산하였다. 제안한 복합 반응면 기법을 이용하여 파괴확률을 계산한 결과 일반적인 반응면 기법보다 향상된 성능을 나타내었다.

• 대한기계학회논문집
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• 제16권9호
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• pp.1643-1653
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• 1992

본 연구에서는 해석적 모우드해석 결과인 모우드 형상벡터를 이용하여 효과적 인 가진점과 응답측정점을 선정하는 기존의 두 방법에 대해 간략히 기술하고 비교검토 하고자 하였다. 첫번째 방법은 주파수응답함수에서 관심있는 모우드의 공진피크치와 관련있는 모우드상수를 이용하는 것이고, 두번째 방법은 계의 관심있는 모우드에 대한 동적 특성을 가장 잘 나타낼 수 있도록 특이치분해(singular value decomposition) 기 법을 적용함으로써 계의 대표자유도(master degree of freedom) 지점들을 선저하는 것 이다.우선 단순한 계인 외팔보아 알루미늄평판에 대해 두 방법을 적용함으로써 비 교검토하였고, 이 결과로부터 두번째 방법의 우수성을 확인할 수 있었다. 이에 따라 보다 복잡한 형상을 갖는 승용차의 부분구조물인 조향휠고정대 (deck cross member : DCM)에 대해서 두번째 방법을 이용하여 모우드 시험을 수행하고 그 결과에 대하여 논 하였다.

• Journal of the Korean Data and Information Science Society
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• 제27권1호
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• pp.111-120
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• 2016

대부분의 불연속 회귀함수의 커널추정량은 알고 있거나 추정된 불연속점을 기준으로 자료를 분리하여 각각을 독립적으로 회귀함수를 적합하고 있다. 회귀모형에서 분산함수가 불연속점을 가지고 있을 때에도 잔차제곱들을 이용하여 위와 같은 불연속 회귀함수의 커널추정법을 활용하고 있다. Kang 등 (2000)은 $M{\ddot{u}}ller$ (1992)의 불연속점과 점프크기 커널추정량을 이용하여 반응변수의 표본을 연속인 회귀함수로부터 표본인 것처럼 수정하여 불연속 회귀함수를 추정하였다. 본 연구에서는 불연속 분산함수를 추정하기 위하여 Kang 등 (2000)의 방법을 이용한다. Kang과 Huh (2006)의 분산함수의 불연속점과 점프크기 추정량으로 잔차제곱들을 수정하고, 수정된 잔차제곱들을 이용하여 불연속 분산함수 커널추정량을 제안할 것이다. 제안된 추정량의 적분제곱오차의 수렴속도를 보여주고 모의실험을 통하여 기존의 추정량과 제안된 추정량을 비교하고자 한다.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2000년도 추계 학술대회논문집
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• pp.46-53
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• 2000

To improve the performance at all design points, multi-point optimization method is implemented for the nose fairing shape design of space launcher. The response surface method is used to effectively reduce the huge computational loads during the optimization process. The drag is selected as the objective function, and the surface heat transfer characteristics, and the internal volume of the nose fairing ate considered as design constraints. Full Wavier-Stokes equations are selected as governing equations. Two points drag minimization, and two points drag / heat flux optimization were successfully performed and configurations which have good performance for the wide operation range were derived. By considering three design points, the space launcher shape which undergoes the least drag during whole flight mission was designed. For all the design cases, the constructed response surfaces show good confidence level with only 23 design points with the proper stretching of the design space.

• 한국정밀공학회지
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• 제19권6호
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• pp.109-118
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• 2002

The vibrational intensity and the dynamic response of a compound vibratory system had been controlled actively by means of a feedforward control method. A compound vibratory system consists of a flexible beam and two discrete systems - a vibrating source and a dynamic absorber. By considering the interactive motions between discrete systems and a flexible beam, the equations of motion for a compound vibratory system were derived using a method of variation of parameters. To define the optimal conditions of a controller the cost function, which denotes a time averaged power flow, was evaluated numerically. The possibility of reductions of both of vibrational intensity and dynamic response at a control point located at a distance from a source were fecund to depend on the positions of a source, a control point and a controller. Especially the presence of a dynamic absorber gives the more reduction on the dynamic response but the less on the vibrational intensity than those without a dynamic absorber.

• 한국유체기계학회 논문집
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• 제11권2호
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• pp.38-45
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• 2008

This study presents a numerical procedure to optimize the compressor design to increase the surge margin of compressor with response surface method (RSM). The Box-Behnken design method is used to reduce the number of calculation for fitting the second-order response surface. In order to consider the increase of surge margin during numerical optimization without any calculation at the surge point, the slope of compressor characteristic curve at the design point is suggested as an objective function in the present optimization problem. Mean line performance analysis method is used to get the design and off-design characteristic curves of centrifugal compressor. The impeller exit angle, impeller exit height and impeller radius are chosen as design variables. The optimum shapes show the increase of surge margin for the surge margin optimization and increase of efficiency for the efficiency optimization in comparison with an initial shape.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2003년도 추계학술대회논문집
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• pp.831-835
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• 2003

The objective of this paper is to suggest an experimental technique to measure the out-of-plane vibration intensity of a coupled plate. In order to measure the out-of-plane vibration intensity of the plate, the frequency response technique has been implemented. In this technique, the 2-D intensity vector at a measurement point has been estimate from the frequency response functions measured at 4 points in the neighborhood of the measurement point. The experimental result has been compared with a theoretical result. It showed that the experimental technique can be effectively used to measure the out-of-plane vibration intensity of plates.