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김상덕,송동주,Kim, Sang-Dug,Song, Dong-Joo 한국유체기계학회 1999 한국유체기계학회 논문집 Vol.2 No.1
CSCM upwind flux difference splitting compressible Navier-Stokes method has been used to predict the transonic flows in a centrifugal compressor diffuser. The modified cyclic. TDMA and the mass flux boundary conditions were used as boundary conditions of the diffuser analysis. Broad flow separation on the suction surface near the hub and shroud was observed from the results of the mass flow rates 5.8, 6.0 and 6.2kg/s at 27000 rpm. The three-dimensional flow analysis predicted successfully that the static pressure increased and the total pressure decreased through the flow passage of the channel diffuser when compared to two-dimensional analysis due to the strong effect of the three-dimensional flow. The mass averaged loss coefficients and pressure coefficients were also studied.
김상덕,Kim, Sang-Dug 한국항공운항학회 2016 한국항공운항학회지 Vol.24 No.4
A primary benefit of flight at high angle-of-attack conditions is to be able to reduce the speed of flight and maneuvers, which can enhance the capability of sensing and obstacle avoidance for a small UAV. The flight at high angle-of-attack conditions, however, is easy to be beyond stall which is characterized by substantial flow separation over an airfoil. Current numerical analysis was conducted on the capabilities of three representative turbulence models to predict the aerodynamic characteristics of a typical airfoil at angle-of-attack conditions. The investigation shows that these turbulence models provide good comparison with experimental data for attached flow at moderate angle-of-attack conditions. Calculation by current turbulence models are, however, not appropriate at high angle-of-attack conditions with flow separation.
김상덕,Kim, Sang-Dug 한국항공운항학회 2015 한국항공운항학회지 Vol.23 No.4
The cyclone separator is a simple device, which causes the centrifugal separation of materials such as droplets or particles in a fluid stream. The cyclone separator utilizes the energy obtained from fluid pressure and linear motion to create rotational fluid motion. This rotational motion leads the materials suspended in the fluid to separate from the fluid quickly due to the centrifugal force. The rotation is produced by the tangential or involuted introduction of fluid into the vessel. These materials may be droplets of fuel in blow-by gas through an engine. Droplets suspended in the feed liquid may separate according to size, shape, or density. And the change of part dimension in a cyclone separator can yield the its performance variation. The current study shows the influence of design parameters on the performance of a cyclone separator for blow-by gas.
김상덕(Sang Dug Kim),송동주(Dong Joo Song) 한국유체기계학회 1998 유체기계 연구개발 발표회 논문집 Vol.- No.-
CSCM upwind flux difference splitting compressible Navier-Stokes method has been used to predict the transonic flows in centrifugal compressor diffuser. The modified cyclic TDMA and the mass flux boundary conditions were used as boundary conditions of the diffuser analysis. With the mass flux boundary condition and the 130×80×40 grid, the compressible upwind Navier-Stokes method predicted the transonic diffuser flowfield successfully. Flow changes in the impeller exit region due to the strong interaction between impeller exit and vaned diffuser, broad flow separation on the suction surface near hub and shroud was observed from the results of the mass flow rates 6.0 and 6.2㎏/s at 27000 rpm. The static pressure increased and the total pressure decreased through the flow passage of the channel diffuser, which were predicted better from the three-dimensional analysis than from the two-dimensional analysis due to the strong effect of the three-dimensional flow. The mass averaged loss coefficients and pressure coefficients were also studied.
3차원 천음속 원심압축기 디퓨저의 탈설계 성능에 관한 수치적 연구
김상덕(Sang Dug Kim),송동주(Dong Joo Song) 한국유체기계학회 1999 유체기계 연구개발 발표회 논문집 Vol.- No.-
A three-dimensional CSCM upwind flux difference splitting Navier-Stokes code with two-equation turbulence models was developed to predict the transonic flows in centrifugal compressor diffuser. The k-ε model of Abe et al. performed well in predicting the pressure distribution in the shock wave/turbulent boundary-layer interaction. Three turbulence models predicted the similar distribution of static pressure through the diffuser and showed a good agreement with the experimental results. The secondary flows in the corner were predicted well by these turbulence models. The pressure increase before the throat of the diffuser vane is important for the overall pressure recovery. As the mass flow rate increased, the blockage decreased at the throat. The pressure coefficient distribution through the diffuser depended on the throat blockage, not on the rotational speed of the impeller.
자가치료용 마이크로캡슐 제조공정 최적화를 위한 교반속도 영향 연구
윤성호(Sung-Ho Yoon),김상덕(Sang-Dug Kim) 한국항공우주학회 2006 韓國航空宇宙學會誌 Vol.34 No.3
교반기 내에서의 교반속도 변화에 따라 제조된 자가치료용 마이크로캡슐의 물리적 특성을 입도분석기와 광학현미경을 통해 실험적으로 관찰하였다. 또한 자가치료용 마이크로캡슐의 제조공정을 이해하기 위해 3차원 수치해석의 수행을 통해 교반기 내에서의 유동특성을 조사하였다. 연구결과에 따르면, 교반기 내에서의 교반속도는 마이크로캡슐의 크기를 결정하는 주요 인자임을 확인하였다. 액체가 혼합된 교반기 내에서는 회전하는 임펠러에 의해 제트와 끝단 와류 성분이 발생하였으며 임펠러의 블레이드 주위에 형성되는 와도는 교반속도가 높아질 때 증가함을 알 수 있었다. 또한 자가치료용 마이크로캡슐의 크기는 끝단 와류와 같은 작은 크기의 혼합 패턴 유동에 큰 영향을 받았다. The physical characteristics of autonomic microcapsules manufactured with various agitation speeds in a stirred tank were observed experimentally by a particle size analyzer and an optical microscope. The flow characteristics in a stirred tank were also investigated through a 3-dimensional numerical simulation to understand the manufacturing process of autonomic microcapsules. According to the results, we found that the agitation speed was the important factor to determine the sizes of microcapsules. The impeller-induced flow allowed the jet and tip-vortex pair components in the mixed fluid of a stirred tank. The vorticity around the blades in the impeller was increased as increasing the agitation speed. In addition, the size of autonomic microcapsules was strongly affected on the small scale mixing pattern such as a tip-vortex pair.