• Transactions of the Korean Society of Mechanical Engineers B
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• v.32 no.4
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• pp.300-306
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• 2008

In the present study, the second order response surface method (RSM) is carried out to get optimum thermal design for enhancing heat transfer in a square channel with bleed flow. The RSM is used as an optimization technique. To calculate the heat transfer, RNG k-epsilon model and enhanced wall function are used. To design optimum rib turbulators, two design variables such as attack angle of rib $({\alpha})$ and rib pitch-to-rib height ratio (p/e) are optimized. In these analyses, the channel inlet Reynolds number was fixed at 10,000 in both non-bleeding and bleeding cases. The response surfaces of two design variables are constructed in cases with and without bleed flow. As a result, the optimum (or highest) heat transfer values are almost the same in ranges of two cases with and without bleed flow. However, the friction losses in the case with bleed flow are lower than those without bleed flow.

• Proceedings of the Korean Vacuum Society Conference
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• 2014.02a
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• pp.197.2-197.2
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• 2014

그래핀(graphene)의 라만 스펙트럼은 전하밀도(charge density)와 기계적 변형(strain)에 민감하여 연구에 널리 활용되고 있다. 본 연구에서는 기계적 박리법으로 만든 그래핀에 황산 수용액으로 p-형 화학도핑(chemical doping)을 유발시키고 전하밀도의 변이에 따른 라만 스펙트럼의 변화를 조사하였다. 이러한 변화를 통해 황산과 물 분자의 계면 확산을 이해하고, $SiO_2/Si$ 기판의 화학적 특성이 미치는 영향을 파악하고자 하였다. 분자의 효율적인 계면 확산을 위해 고온 산화반응을 이용하여 그래핀의 기저면에 나노공(nanopore)을 만든 후, 액상에서 라만 스펙트럼을 측정하였다. 증류수 속에 담궜을 때 물 분자가 그래핀-기판 계면 사이로 확산되면서 열처리에 의해 유발된 정공이 사라짐을 확인하고, D-봉우리의 가역적인 변화로부터 그래핀의 구조적 변화를 유추하였다. 황산 농도를 증가시켰을 때 G와 2D-봉우리의 진동수가 상호간에 일정한 비율로 증가하여 정공의 밀도가 증가함 알 수 있었다. 동일한 시료에 대해 황산의 농도를 감소시킴으로써 p-형 도핑을 제거하고 동일한 반응을 가역적으로 반복할 수 있었다. 상기한 분자의 2차원 확산 현상은 나노공의 유무와 기판의 전처리 조건에 따라 크게 달라진다는 사실을 확인 할 수 있었다. 또한 여러 파장에서 측정된 전하밀도와 기계적 변형에 의한 G와 2D-봉우리의 진동수 변화로부터 다른 연구자들이 활용할 수 있는 검정곡선을 제시하였다.

• Korean Journal of Materials Research
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• v.8 no.9
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• pp.791-796
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• 1998

self-aligned silicide(salicide)제조시 CoSi2의 에피텍셜 성장을 돕기 위하여 Co와 Si 사이에 내열금속층을 넣은 Co/내열금속/Si의 실리사이드화가 관심을 끌고 있다. Hf 역시 Ti와 마찬가지로 이러한 용도로 사용될 수 있다. 한편, Co/Hf 이중층 salicide 트랜지스터가 성공적으로 만들어지기 위해서는 spacer oxide 위에 증착된 Co/Hf 이중층이 열적으로 안정해야 한다. 이러한 배경에서 본 연구에서는 SiO2기판 위에 증착한 Co 단일층과 Co/Hf 이중층을 급속열처리할 때 Co와 SiO2간의 계면과 Co/Hf와 SiO2간의 계면에서의 상호반응에 대하여 조사하였다. Co 단일층과 Co/Hf 이중층은 각각 $500^{\circ}C$와 $550^{\circ}C$에서 열처리한 후 면저항이 급격하게 증가하기 시작하였는데, 이것은 Co층이 SiO2와의 계면에너지를 줄이기 위하여 응집되기 때문이다. 이 때 Co/Hf의 경우 열처리후 Hf에 의하여 SiO2 기판이 일부 분해됨으로써 Hf 산화물이 형성되었으나, 전도성이 있는 HfSix 등의 화합물은 발견되지 않았다.

• Proceedings of the KIEE Conference
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• 2002.07c
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• pp.1470-1472
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• 2002

3원계 51wt%Ni-4lwt%Cr-8wt%Si 합금 타겟을 가지고 DC/RF 마그네트론 스퍼터를 이용하여 박막저항을 제조하였고, 낮은 저항온도계수(TCR)를 가지는 박막을 만들기 위해 제조공정의 변화에 따른 박막의 미세구조와 전기적인 특성을 조사하였다. 스퍼터링 제조공정 변수로써 DC/RF Power, 반응압력, 기판온도를 변화시켰고, 제조된 박막은 공기중에서 $400[^{\circ}C]$까지 열처리 하였다. 반응압력을 감소시킴에 따라 TCR값은 감소하였고, 기판온도 및 열처리 온도의 증가에 따라 TCR값도 증가하였다. 또한, 비저항은 DC Power에서 $172[{\mu}{\Omega}cm]$, RF인 경우에는 $209[{\mu}{\Omega}cm]$을 나타내었고, 각각 +52, $-25[ppm/^{\circ}C]$의 TCR값을 나타냈다. 이와 같은 결과로부터 제조공정을 변화시킴에 따라 면저항 및 저항온도계수의 제어가 가능함을 알 수 있었다.

• The Korean Journal of Applied Statistics
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• v.20 no.1
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• pp.133-145
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• 2007

Local linear estimator has a number of advantages over the traditional kernel estimators. The better performance near boundaries is one of them. However, local linear estimator can produce erratic result in sparse regions in the realization of the design and to solve this problem much research has been done. Local linear quasi-likelihood estimator has many common properties with local linear estimator, and it turns out that sparse design can also lead local linear quasi-likelihood estimator to erratic behavior in practice. Several methods to solve this problem are proposed and their finite sample properties are compared by the simulation study.

• Transactions of the Korean Society for Noise and Vibration Engineering
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• v.16 no.5 s.110
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• pp.485-494
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• 2006

The state-of-the-art of low-noise fan design usually includes the consideration of optimal sound level and sound quality. The influential design parameters of the noise level by the centrifugal fan were selected based on the preliminary test. The centrifugal fans were designed according to the experiment plan method by specifying the selected design parameters. The experiment with these machined mock-up's of centrifugal impellers suggested the major design parameters among many, having impacts upon the indices of sound quality (e.g. loudness, sharpness, roughness and fluctuation strength) at the same operation point. With the response surface method, the major design parameters selected thereafter were analyzed to estimate each contribution upon the sound quality of the centrifugal fan, and the optimal values were drawn by the consideration of the sound quality levels and their regression equations. In addition, the validity of the regression equations was numerically verified by means of the coefficient of determination. Furthermore, the mechanism by which the centrifugal fan impeller influences the determinants of its sound quality was suggested.

• Water for future
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• v.29 no.2
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• pp.143-151
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• 1996

The dynamic responses in the subsurface outflow, surface saturation area, soil moisture storage are established by numerical experiments with Richards equation. In addition to this, the dynamical relationship between surface saturation area and subsurface outflow, and between surface saturation area and soil moisture storage are also determined by varying the hillslope shape, soil type, and boundary condition. The simulation results indicate that the dynamical relationships between surface saturation area and subsurface outflow, and between surface saturation area and soil moisture storage are approximated by the steadystate relationships. And the dynamic responses of subsurface outflow and surface saturation area are characterized by the double peaks although the rainfall pattern is asimple pulse input. As a result of numerical simulation, the physical mechanism for the occurrence of the double peaks is explained using the concept of variable source area.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.30 no.1
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• pp.9-19
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• 2002

Accuracy of AUSM-type schemes is closely related to a speed of in a cell-interface. Effect to accuracy by a speed of sound invastigated in the region of subsonic, transonic, and supersonic flows repectively. The advantage of the speed of sound in AUSMPW+ are summerized as the improvement of accuracy in capturing an oblique shock and the removal of an expansion shock to satisfy the entropy condition. They are proven by mathmatics and numerical result. Moreover AUSMPW+ is extended to a real gas flow and the speed of sound for equilibrium and nonequilibrium gas which could give exact soultions in an oblique shock is proposed.

• The KSFM Journal of Fluid Machinery
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• v.17 no.1
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• pp.28-34
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• 2014

This paper presents the performance enhancement of a double-inlet centrifugal blower by the shape optimization of an impeller. Two design variables, a number of blade and a length of chord, are introduced, and analyzed by a response surface method. Three-dimensional compressible Navier-Stokes equations are used to analyze the blower performance and the internal flow of the blower. Throughout the numerical simulation of the blower, blower efficiency can be increased by reducing separation flow generating from the blade leading edge of a blade pressure surface. It is noted that recirculation flow observed inside the blade passage induces low velocity region, thus increases pressure loss. Efficiency and pressure of the optimum blower are successfully increased up to 3% and 3.9% compared to those of reference blower at the design flow condition, respectively. Detailed flow field inside the blower is also analyzed and compared.

• Proceedings of the KSME Conference
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• 2004.04a
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• pp.1726-1731
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• 2004

This paper presents the response surface optimization method using three-dimensional Navier-Stokes analysis to optimize the shape of a forward-curved blades centrifugal fan. For numerical analysis, Reynolds-averaged Navier-Stokes equations with $k-{\varepsilon}$ turbulence model are discretized with finite volume approximations. In order to reduce huge computing time due to a large number of blades in forward-curved blades centrifugal fan, the flow inside of the fan is regarded as steady flow by introducing the impeller force models. Three geometric variables, i.e., location of cut off, radius of cut off, and width of impeller, and one operating variable, i.e., flow rate, were selected as design variables. As a main result of the optimization, the efficiency was successfully improved. And, optimum design flow rate was found by using flow rate as one of design variables. It was found that the optimization process provides reliable design of this kind of fans with reasonable computing time.