• 한국해양환경ㆍ에너지학회지
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• 제13권4호
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• pp.241-248
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• 2010

본 논문은 조류발전을 위하여 가장 보편적으로 사용되는 수직축 조류발전 터빈의 하나인 다리우스 터빈의 효율에 미치는 다양한 설계변수의 영향을 살펴보기 위하여 수행하였다. 날개 수, 코드 길이, 피치 및 캠버를 설계변수로 채택하였으며, 2차원 및 3차원 비정상 난류유동해석을 위하여 FLUENT의 RANS방정식과 k-e 난류모델을, 격자계 모델링을 위하여 GAMBIT을 이용하였다. 기본적인 수치해석방법은 정현주 등(2009)을 참조하였다. 설계변수 변경에 따른 방대한 계산 량을 감안하여 수치해석의 신뢰도가 허락하는 범위에서 대부분 2차원 해석으로 결과를 도출하였다. 본 연구에서 제시한 설계변수의 최적화를 통하여 기준모형보다 월등한 성능을 보이는 고효율 수직축 터빈 모델을 제시할 수 있었다.

• 대한조선학회논문집
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• 제53권5호
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• pp.343-352
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• 2016

In this study, a pre-swirl duct for the 180,000 DWT bulk carrier has been designed from a propulsion standpoint using CFD. The stern duct - designed by NMRI - was selected as the initial duct. The objective function is to minimize the value of delivered power in model scale. Design variables of the duct include duct angle, diameter, chord length, and vertical and horizontal displacements from the center. Design variables of the stators are blade number, arrangement angle, chord length, and pitch angle. A parametric design was carried out with the objective function obtained using CFD. Reynolds averaged Navier-Stokes equations have been solved; and the Reynolds stress model applied for the turbulent closure. A double body model is used for the treatment of free-surface. MRF and sliding mesh models have been applied to simulate the actuating propeller. A self-propulsion point has been obtained from the results of towing and self-propelled computations, i.e., form factor obtained from towing computation and towing forces obtained from self-propelled computations of two propeller rotating speeds. The reduction rate of the delivered power of the improved stern duct is 2.9%, whereas that of the initial stern duct is 1.3%. The pre-swirl duct with one inner stator in upper starboard and three outer stators in portside has been designed. The delivered power due to the designed pre-swirl duct is reduced by 5.8%.

• 한국해양공학회지
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• 제30권2호
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• pp.125-133
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• 2016

In this paper, we propose a vertical axis water turbine with dual blades. A parametric study was conducted using numerical analyses. First, a two-dimensional finite-volume analysis with a commercial code was used to find the pitch angle of the main blade under different tip speed ratio conditions. Second, we developed a potential-based panel method to find the best configuration of the inner blades. Experimental tests were conducted at the circulating water channel of Chungnam National University. Various configurations of the dual blades were considered, and their performances were comparatively investigated. The results showed that the turbine with movable dual blades produces a constant torque and tip speed ratio at various flow rates.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2004년도 추계학술발표대회 논문집
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• pp.125-130
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• 2004

This study proposes a development for the l-kW class small wind turbine system, which is applicable to relatively low wind speed region like Korea and has the variable pitch control mechanism. In the aerodynamic design of the wind turbine blade, parametric studies were carried out to determine an optimum aerodynamic configuration which is not only more efficient at low wind speed but whose diameter is not much larger than similar class other blades. A light composite structure, which can endure effectively various loads, was newly designed. In order to evaluate the structural design of the composite blade, the structural analysis was performed by the finite element method. Moreover both structural safety and aerodynamic performance were verified through the prototype test.

• International Journal of Aerospace System Engineering
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• 제2권2호
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• pp.83-86
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• 2015

Taking the four-wheel bogie landing gear as an example, the force status of truck-like landing gear during the landing impact was analyzed and the simulation model of four-wheel bogie landing gear was established. Firstly, a landing gear prototyping model was established using CATIA and imported to LMS Virtual.lab. Secondly, dynamic analysis of the landing impact was simulated with the established model. Finally, with the help of LMS Virtual.lab's parametric design ability, the effects of landing approach and truck pitch angle on the landing performance, truck motion and truck beam strength were studied. These conclusions will be useful to the design and analysis of the truck.

• 한국철도학회:학술대회논문집
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• 한국철도학회 2006년도 추계학술대회 논문집
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• pp.1293-1298
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• 2006

A numerical analysis was performed to verify how much additional force is induced by short or long pitch rail corrugations in track. The rail corrugations assumed as sine wave having various pitches and depths. The variation of wheel force, displacement and acceleration of rail and sleeper was investigated. In the results, it was shown that each item of the investigation was increased as the pitches and depths become large. It is expected that the results of the parametric study can be used as a preliminary data for the determination of economical maintenance criteria for rail corrugation in the future

• Wind and Structures
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• 제28권3호
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• pp.191-201
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• 2019

In this paper, the aerodynamic analysis of a vertical axis wind turbine was carried out by CFD approach to optimize the turbine performance. To perform numerical simulation, SST-Transition turbulence model was used, which demonstrated more precise results compared to non-transition models. A parametric study was conducted to optimize the VAWT performance based on the selected model. The investigation of pitch angle changes showed that the highest power produced by the turbine occurs at $2^{\circ}$ angle. Considering the effect of the rotor's arm junction to the airfoil showed that by increasing the distance of the junction from the edge of the airfoil from 25 cm to 40 cm, the power of the turbine increases by 60%. However, further increase in this distance results in power decrease. Based on the proposed numerical model, a case study was conducted to consider the installation of four VAWTs in the southwest corner of the medical science building at TMU campus with a height of 42m. The results of the simulation showed that 8.27 MWh energy is obtainable annually.

• 대한의용생체공학회:의공학회지
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• 제16권1호
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• pp.95-100
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• 1995

본 논문에서는 발성기관인 후두(glottis)의 기능을 평가하기 위하여 후두신호의 주파수 변동과 진폭변동의 영향을 분석하였다. 정상인의 EGG(electroglottograph)신호는 매개변수 방법을 이용하여 최적의 차수가 9차인 자귀회귀형 모델로 설명할 수 있으며, 이것은 전달함수를 결정함으로써 해석이 가능하다. EGG신호의 진푹과 주파수의 변동은 변복조방식의 4전극 EGG 시스템으로 얻어지며, 후두기능 상태식별을 목적으로 개발하였다. EGG를 이용하여 후두의 닫힘구간과 열림구간을 계산함으로써 비정상 EGG신호는 비주기적이며 불안정한 상태라는 것을 구별할 수 있었다. 정상과 비정상의 피검자들을 구분할 수 있는 파라미터인 주파수 변동은 정상인의 m$\pm$0.5*sd이고, 진폭변동은 m$\pm$2*sd가 각각 되었다. 또한 EGG신호를 Hillbert 변환함으로써 얻어진 궤적의 패턴을 이용하여 정상과 비정상의 후두기능상태를 효과적으로 분류할 수 있었다.

• 한국전산유체공학회지
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• 제21권1호
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• pp.78-85
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• 2016

While most AUV researches have concerned about single hydrofoil, practical AUV's are generally operated with multiple hydrofoils. Double hydrofoil study attempts to evaluate thrust and efficiency with various flapping motions, and carries out design optimization using parametric analysis. Flow patterns such as vortex shedding and wake-body interaction are carefully investigated during design variable sensitivity analysis. The purpose of this design optimization is to find out the optimal motion that yields maximum thrust and efficiency. The design optimization employes several techniques such as table of orthogonal arrays, Kriging method, ANOVA analysis and MGA. Throughout this research, it is possible to find the optimal values of heaving ratio, heaving shift and pitch shift: Heaving ratio 0.950, heaving shift $23.120^{\circ}$ and pitch shift $89.991^{\circ}$ are found to be optimal values in double hydrofoil motions. Thrust and efficiency are 16.7% and 35.1% higher than existing AUV that did not consider nonlinear dependency of motion parameters. This results may offer an effective framework that is applicable to various AUV motion analyses and designs.

• 에너지공학
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• 제12권2호
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• pp.84-92
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• 2003

구리밀봉 증기발생기의 열적크기 계산을 위한 1차원 열수력코드를 개발하였다. 고온 및 저온측 전열관사이의 구리의 열전도는 1차원으로 가정하고, 전열관 피치의 함수로 열저항을 구하였다 물/증기측 유동영역은 아냉, 포화핵비등, 포화막비등, 과열영역의 4 구간으로 구분하였다. 매개변수 연구를 위한 전열관 갯수는 250에서 3500이며, P/D비율은 각각1.4, 1.6, 1.8로 하였다. 계산결과, 전열관 갯수가 2500일 때 전열관 길이는 약 12 m, 직경은 약 3 m이다. P/D를 증가시키면 구리에 의한 열저항 성분이 증가하지만 전열관 길이는 큰 차이가 없음을 알 수 있었다.