• 한국해양공학회지
• /
• 제31권4호
• /
• pp.281-287
• /
• 2017

In the case of fixed offshore wind turbines, scouring phenomena have been reported around sub-structures as a result of currents, which seriously damage the structural stability. A parametric study of the various sub-structures of a fixed offshore wind turbine was performed to investigate their effects on the scouring phenomena. For a suction bucket foundation and monopile, the effects of the stick-up heights and water depth were studied, respectively. The open source libraries, called OpenFOAM, were used to simulate a violent flow around a foundation. The numerical methods were selected based on a two-dimensional analysis of a suction bucket. Based on the results for various stick-up heights, a larger scouring region was observed with an increase in the stick-up height because of the down-wash flow around a foundation. Based on the results for various monopile water depths, the water depth had an insignificant effect on the scouring.

• 대한기계학회논문집B
• /
• 제20권7호
• /
• pp.2267-2276
• /
• 1996

공정산업분야 및 분무연소분야에서 많이 사용되고 있는 2유체 분무기에서 출구 초음속유동의 가시화와 하류의 가스압력 측정 결과로부터 다음과 같은 결론을 얻었다. 1) 과소팽창 또는 과대팽창 초음속노즐 유동에서 출구 Mach수가 일정한 경우, 유동이 박리하지 않는다면 가스의 정체압력(유량)이 증가함에 따라 노즐출구에서 충돌정체점까지의 길이와 초음속 유동영역의 길이는 증가한다. 2) 스피팅 현상은 액체공급관 출구의 흡인압력은 분사가스압력이 증가함에 따라 단조증가하지만 분사가스압력이 0.5MPa이상이 되면 증감현상이 커지며 돌출형 노즐에서 유동박리시 급격히 증가한 다음 거의 일정하게 유지된다. 4) 액체공급관 하류축상의 압력변화는 출구의 음압에서 충돌정체점까지 상승한 다음 급강하하고 충격파 세포상의 구조에 따라 진동하면서 대기압에 도달한다.

• 한국산학기술학회논문지
• /
• 제19권3호
• /
• pp.679-686
• /
• 2018

지하철 터널 내에 축적된 미세먼지와 초미세먼지를 제거하기 위해서는 새로운 형식의 분진흡입차량이 필요하다. 따라서 최근 개발된 분진흡입차는 초미세먼지 제거를 위한 흡입시스템과 사이클론형식의 전처리부 및 전기집진기를 장착하고 있다. 본 논문에서는 집진차량의 하부에 설치된 먼지 흡입시스템이 다양한 크기의 먼지입자를 효과적으로 흡입하고 처리하기 위해 사이클론형식의 전처리부가 포함된 집진시스템을 설계하고 집진효율을 ANSYS FLUENT의 전산유체해석을 통해 확인하였다. 흡입구와 사이클론형 프리필터가 연결된 격자모델을 기반으로 공기유동과 상차분모델(Discrete Phase Model)을 이용하여 다양한 입자의 크기와 종류 및 흡입팬의 용량에 따른 입자의 거동을 해석하였다. 다양한 입자의 크기와 종류, 흡입팬의 용량에 대해서 해석결과 집진차량의 운영속도 5km/h에서 미세먼지처리를 위해서는 흡입팬의 용량 $1500m^3/min$에서 흡입구가 궤도면으로부터 약 100mm이내일 때 $100{\mu}m$ 이하 크기의 먼지를 모두 처리할 수 있음을 확인하였다. 이러한 흡입구와 사이클론형식의 프리필터를 탑재한 터널집진차량은 후단에 설치된 전기집진기의 부하를 줄이고, 지하 터널내의 미세먼지와 초미세먼지의 제거에 효과적으로 활용될 수 있을 것으로 기대된다.

• 유체기계공업학회:학술대회논문집
• /
• 유체기계공업학회 2005년도 연구개발 발표회 논문집
• /
• pp.359-364
• /
• 2005

Centrifugal pump shows the strongest secondary flow. Wake is formed near pressure surface close to hub at impeller exit for centrifugal pump impeller. Pressure gradient drives secondary flow in the inducer region, while in the remaining region the following sources drive together: > Pressure gradient > Coriolis force Low-momentum fluid near suction surface hub moves toward pressure surface hub in mixed-flow pump impeller. Tip leakage vortex dominate secondary flow in axial-flow pump impeller. Tip leakage vortex dominate secondary flow in axial-flow in axial-flow pump impeller

• Journal of Mechanical Science and Technology
• /
• 제20권4호
• /
• pp.569-579
• /
• 2006

In the present study, the unsteady Couette flow with heat transfer of a dusty viscous incompressible electrically conducting fluid under the influence of an exponential decaying pressure gradient is studied without neglecting the Hall effect. The parallel plates are assumed to be porous and subjected to a uniform suction from above and injection from below while the fluid is acted upon by an external uniform magnetic field is applied perpendicular to the plates. The governing equations are solved numerically using finite differences to yield the velocity and temperature distributions for both the fluid and dust particles.

• Journal of Mechanical Science and Technology
• /
• 제20권8호
• /
• pp.1232-1239
• /
• 2006

In the present study, the unsteady Hartmann flow with heat transfer of a viscous incompressible electrically conducting fluid under the influence of an exponentially decreasing pressure gradient is studied. The parallel plates are assumed to be porous and subjected to a uniform suction from above and injection from below while the fluid is acted upon by an external uniform magnetic field applied perpendicular to the plates. The equations of motion are solved analytically to yield the velocity distributions for both the fluid and dust particles. The energy equations for both the fluid and dust particles including the viscous and Joule dissipation terms, are solved numerically using finite differences to get the temperature distributions.

• 유체기계공업학회:학술대회논문집
• /
• 유체기계공업학회 2004년도 유체기계 연구개발 발표회 논문집
• /
• pp.517-520
• /
• 2004

• Journal of Advanced Marine Engineering and Technology
• /
• 제38권1호
• /
• pp.31-38
• /
• 2014

이젝터는 고압의 주유동을 통해 저압의 부유동을 이동시키는 단순한 장치이다. 이젝터의 효율은 주방향으로 작동하는 다른 이송 장치에 비해 매우 낮다. 그러나 구동장치가 없어 간단한 구조를 가지고 있으며, 낮은 구동에너지로 많은 양의 유체를 이송시킬 수 있는 장점을 가지고 있다. 본 연구에서는 선박에서 많이 사용되고 있는 side-type 액체용 이젝터에 작동유체의 유량을 변화시키면서 정상, 비압축성 유동에 대해 실험 및 CFD 분석을 통하여 직관부 및 디퓨저의 길이변화에 따른 이젝터의 유동 패턴과 흡입 현상을 분석하였다.

• International Journal of Fluid Machinery and Systems
• /
• 제6권2호
• /
• pp.56-74
• /
• 2013

Stall stagnations in the system of axial-flow compressors and ducts occur in transition from deep surge conditions to decayed or converged stall conditions. The present study is concerned with the boundaries between the deep surges and the stagnation stalls on the basis of analytical results by a code on surge transients analysis and simulation. The fundamental acoustical-geometrical stagnation boundaries were made clear from examinations of the results on a variety of duct configurations coupled with a nine-stage compressor and a single stage fan. The boundary was found to be formed by three parts, i.e., B- and A-boundaries, and an intermediate zone. The B-boundary occurs for the suction-duct having a length of about a quarter of the wave-length of the first resonance in the case of very short and fat plenum-type delivery duct. On the other hand, the A-boundary occurs for the long and narrow duct-type delivery flow-path having a length about a fifth of the wavelength and relatively small sectional area in the case of short and narrow suction ducts. In addition to this, the reduced surge-cycle frequencies with respect to the duct lengths are observed to have respective limiting values at the stagnation boundaries. The reduced frequency for the B-boundary is related with a limiting value of the Greitzer's B parameter. The tendency and the characteristic features of the related flow behaviors in the neighborhood of the boundaries were also made clearer.

• 한국유체기계학회 논문집
• /
• 제5권3호
• /
• pp.15-24
• /
• 2002

This paper presents an experimental study on the unsteady flow phenomena such as leakage flow and rotating stall which have influences on the performance and stability of an axial flow fan. For this study, unsteady pressure were measured using high frequency pressure transducers mounted on the easing wall of rotor passage and analyzed by Double Phase-Locked Averaging Technique. As the flow rate was reduced to near stall point, the pressure difference between the pressure and the suction side of the blade was increased especially new the leading edge and the lowest pressure zone of suction side was gradually developed. From the result of unsteady pressure field on the casing wall, one period of rotating stall was divided into three zones and the flow characteristics on each zone were described in detail.