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미래 풍력발전산업의 집적지육성을 위한 녹산클러스터 발전방향
임희창,한규택,장광호,진성호,김용환,Lim, Hee-Chang,Han, Gyu-Taek,Jang, Gwang-Ho,Jin, Seong-Ho,Kim, Yong-Hwan 산업클러스터학회 2009 산업클러스터 Vol.3 No.1
현재 풍력에너지는 세계적으로 가장 급격하게 관심이 집중되고 있는 에너지원으로 평가되고 있다. 이러한 환경의 변화와 신재생에너지에의 집중된 관심은 보다 추진력을 얻으며 풍력발전관련 산업체들에 힘을 실어주고 있다. 부산의 녹산 풍력클러스터는 풍력발전기의 요소부품을 생산하는데 있어 주요한 기업체들이 몰려있으며, 과거 몇 년간 세계적인 관심에 편승하여 산업입지가 높아지고 있지만, 이에 반해 관심은 여전히 제한적이었다. 본 논문은 서구에서 이루어지고 있는 풍력발전산업에서 최근까지 이루어졌던 주관심 이슈에 대해 조사하고자 한다. 또한 녹산 풍력클러스터의 현황과 보다 효과적인 집적지를 구성하기 위한 향후 계획에 대한 제안을 하고자 한다.
O-ring을 이용한 원주의 항력감소에 관한 실험적 연구
임희창,이상준,Lim, Hee-Chang,Lee, Sang-Joon 대한기계학회 2003 大韓機械學會論文集B Vol.27 No.8
The flow around a circular cylinder was controlled by attaching O-rings to reduce drag force acting on the cylinder. Four experimental models were tested in this study; one smooth cylinder of diameter D (D=60mm) and three cylinders fitted with O-rings of diameters d=0.0167 D, 0.05D and 0.067 D with pitches of PPD=2D, 1D, 0.5D and 0.25D. The drag force, mean velocity and turbulence Intensity profiles in the near wake behind the cylinders were measured for Reynolds numbers based on the cylinder diameter in the range of Re$_{D}$=7.8$\times$10$^3$~1.2$\times$10$^{5}$ . At Re$_{D}$=1.2$\times$10$^{5}$ , the cylinder fitted with O-rings of d=0.0167D in a pitch interval of 0.25D shows the maximum drag reduction of about 5.4%, compared that with the smooth cylinder. The drag reduction effect of O-rings of d=0.067D is not so high. For O-ring circulars, as the Reynolds number increases, the peak location of turbulence intensity shifts downstream and the peak magnitude is decreased. Flow field around the cylinders was visualized using a smoke-wire technique to see the flow structure qualitatively. The size of vortices and vortex formation region formed behind the O-ring cylinders are smaller, compared with the smooth cylinder.der.
임희창(Hee Chang Lim) 대한기계학회 2006 대한기계학회 춘추학술대회 Vol.2006 No.11
The separated flow around a surface mounted cubic obstacle placed in a deep turbulent boundary layer has been studied with the aim to understand the flow structures responsible for producing extreme suction pressures on the roof of a surface-mounted cube normal to a thick turbulent boundary layer. The experiment includes wind tunnel work with PIV and LDA measurements. The experiments are carried out at Reynolds numbers, based on the velocity U at the cube height h, of 18,600 to 346,000, and large enough that the mean flow is effectively Reynolds number independent. The results include the measurements of the flow fields around the leading edge of the cube, and the separated flows above and behind the cube. The possible relationship between gusts and 3D vortex structure obtained from the numerical simulation will be presented.