• 한국추진공학회지
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• 제22권1호
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• pp.52-57
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• 2018

본 논문에서는 9톤급 다단연소사이클 엔진용 산화제 과잉 예연소기 분사기 설계 및 수류 시험 결과에 대해 기술하고자 한다. 총 3 종류의 동축 와류 분사기를 설계하고 각 종류마다 12개의 분사기를 제작하였다. 연료 접선 홀 직경은 모두 동일하며, 산화제와 연료가 연소되어 발생하는 기체 산화제와 냉각 채널에서 배출되는 액체 산화제 모멘텀의 비에 따라 산화제 과잉 예연소기 분사기의 연소에 어떠한 영향이 있는지를 연구하기 위해 산화제 접선 홀의 직경을 다르게 제작하였다. 추후에 산화제 과잉 예연소기를 이용한 파워팩과 연소시험을 통해 검증될 예정이다. 수류 시험 결과, 연료 유량 및 산화제 접선 홀의 유량값은 설계 차압을 기준으로 목표 유량값에 도달하였다.

• 한국추진공학회지
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• 제11권5호
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• pp.51-59
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• 2007

충돌형 산화제 주입기를 사용한 end-burning 하이브리드 연소기의 혼합특성을 선행 연구되었던 접선형 주입기와 비교 분석하였다. 충돌형 주입기를 사용한 연소유동장이 접선형 주입기에 비해 축방향 및 반경방향으로 월등한 혼합특성과 연소효율을 보였다. 충돌효과와 선회효과를 동시에 발생시키는 파생형 주입기를 사용한 결과, 보다 넓은 연소실 영역에서 혼합효율이 증대되었으며 연료 표면의 연소 균일도가 향상될 수 있음을 확인하였다. 충돌로 인한 축방향 운동량과 선회유동이 체류시간과 난류강도를 증가시켜 혼합을 촉진시키는 주요 인자로 판단되었으나 연소실의 기하학적 형상변화를 꾀한 step의 유무는 난류혼합 증진에 있어서 중요한 변수가 아님을 확인할 수 있었다.

• International Journal of Fluid Machinery and Systems
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• 제5권2호
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• pp.49-59
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• 2012

The present study is devoted to the influence of a superposed radial inflow in a rotor-stator cavity with a peripheral opening. The flow regime is turbulent, the two boundary layers being separated by a core region. An original theoretical solution is obtained for the core region, explaining the reason why a weak radial inflow has no major influence near the periphery of the cavity but strongly affects the flow behavior near the axis. The validity of the theory is tested with the help of a new set of experimental data including the radial and tangential mean velocity components, as well as three components of the Reynolds stress tensor measured by hot-wire anemometry. The theoretical results are also in good agreement with numerical results obtained with the Fluent code and experimental data from the literature.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2003년도 추계학술대회
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• pp.822-827
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• 2003

Experiments were done for the three dimensional unsteady flow in a counter rotating axial flow fan under stable operating condition. Flow fields in a counter rotating axial flow fan were measured at cross-sectional planes of the upstream and downstream of each rotor. Cross sectional flow patterns were investigated through the acquired data by the $45^{\circ}$ inclined hot-wire. Flow characteristics such as tip vortex, secondary flow and tip leakage flow were confirmed through axial, radial and tangential velocity vector plot. Swirl velocity, which was generated by the front rotor, was recovered in the form of static pressure rise by the rear rotor except for hub and tip regions.

• Wind and Structures
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• 제11권2호
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• pp.75-96
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• 2008

A better understanding of tornado-induced wind loads is needed to improve the design of typical structures to resist these winds. An accurate understanding of the loads requires knowledge of near-ground tornado winds, but observations in this region are lacking. The first goal of this study was to verify how well a CFD model, when driven by far field radar observations and laboratory measurements, could capture the flow characteristics of both full scale and laboratory-simulated tornadoes. A second goal was to use the model to examine the sensitivity of the simulations to various parameters that might affect the laboratory simulator tornado. An understanding of near-ground winds in tornadoes will require coordinated efforts in both computational and physical simulation. The sensitivity of computational simulations of a tornado to geometric parameters and surface roughness within a domain based on the Iowa State University laboratory tornado simulator was investigated. In this study, CFD simulations of the flow field in a model domain that represents a laboratory tornado simulator were conducted using Doppler radar and laboratory velocity measurements as boundary conditions. The tornado was found to be sensitive to a variety of geometric parameters used in the numerical model. Increased surface roughness was found to reduce the tangential speed in the vortex near the ground and enlarge the core radius of the vortex. The core radius was a function of the swirl ratio while the peak tangential flow was a function of the magnitude of the total inflow velocity. The CFD simulations showed that it is possible to numerically simulate the surface winds of a tornado and control certain parameters of the laboratory simulator to influence the tornado characteristics of interest to engineers and match those of the field.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 1999년도 제13회 학술강연논문집
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• pp.27-27
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• 1999

To illustrate the global variation of the droplet mean diameters and the turbulent flow characteristics in counterflowing internal mixing pneumatic nozzle, the experimental measurements at five axial downstream locations(i.e., at Z=30, 50, 80, 120, and 170mm) were made using a PDPA(Phase Doppler Particle Analyzer) under the different air injection pressures ranging from 40 ㎪ to 120 ㎪. A nozzle with axi-symmetric tangential-drilled four holes at an angle of 15$^{\circ}$ has been designed and manufactured. The distributions of velocities, turbulence intensities, turbulence kinetic energy, turbulent correlation coefficients, spray angle, droplet mean diameters, volume flux, number density are quantitatively analyzed. It is possible to discern the effects of increasing air pressure. It indicates that the strong axial momentum in spite of more or less disparity between the velocity components means more reluctant to disperse radially, and that axial fluctuating velocities are substantially higher than those of radial and tangential ones, suggesting that the disintegration process is enhanced under higher air assist. The larger droplets are detected in the spray centerline at the near stations and smaller ones are generated due to further subsequent breakup at farther axial locations are attributed to the internal mixing type nozzle characteristics. Despite of the strong axial momentum, the poor atomization around the centre close to the nozzle exit is attributed to the lower rates of spherical particles which are not subject to instantaneous breakup. As it goes downstream, however, substantial increases in SMD(Sauter Mean Diameter) from the central part toward spray periphery are understandable because the droplet relative velocity is too low to bring about any subsequent disintegration.

• 대한기계학회논문집B
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• 제21권5호
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• pp.615-627
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• 1997

An experiment was performed to local heat transfer coefficient and Nusselt number in the circular duct of 180.deg. bend for Re=6*10$^{4}$, 8*10$^{4}$ and 1*10$^{5}$ at swirling flow and non-swirling flow conditions. The test tube with circular section was made by stainless which has curvature ratio 9.4. The wall of test tube was heated directly by electrical power to 3.51 kw and swirling motion of air was produced by a tangential inlet to the pipe axis at the 180 degree. Measurements of local wall temperatures and bulk mean temperature of air are made at four circumferential positions in the 16 stations. The wall temperatures show particularly reduced distribution curve at bend for non-swirling flow but this effect does not appear for swirling flow. Nusselt number distributions for swirling flow which was calculated from the measured wall and bulk temperatures were higher than that of non-swirling flow. Average Nusselt number of swirling flow increased about 90 ~ 100% than that of non-swirling flow whole through the test tube. The Nu/N $u_{DB}$ values at the station of 90.deg. for non-swirling flow and swirling flow are respectively about 2.5 and 4.8 at Re=6*10$^{4}$. Also that is good agreement with Said's result for non-swirling flow. flow.

• 대한조선학회논문집
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• 제55권6호
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• pp.474-481
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• 2018

This paper is to compare by numerical analysis the flow characteristics and propulsion performance of stern with the shape change of K-duct, a pre-swirl duct developed by Korea Research Institute of Ships & Ocean Engineering (KRISO). First, the characteristics of the propeller and the resistance and self-propulsion before and after the attachment of the K-duct to the ship were verified and the validity of the calculation method was confirmed by comparing this result with the model test results. After that, resistance and self-propulsion calculations were performed by the same numerical method when the K-duct was changed into five different shapes. The efficiency of the other five cases was compared using the delivery horsepower in the model scale and the flow characteristics of the stern were analyzed as the velocity and pressure distributions in the area between the duct end and the propeller plane. For the computation, STAR-CCM +, a general-purpose flow analysis program, was used and the Reynolds Averaged Navier-Stokes (RANS) equations were applied. Rigid Body Motion (RBM) method was used for the propeller rotating motion and SST $k-{\omega}$ turbulence model was applied for the turbulence model. As a result, the tangential velocity of the propeller inflow changed according to the position angle change of the stator, and the pressure of the propeller hub and the cap changes. This regulated the propeller hub vortex. It was confirmed that the vortex of the portion where the fixed blade and the duct meet was reduced by blunt change.

• 한국가스학회지
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• 제21권3호
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• pp.53-60
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• 2017

연소로에서 질소산화물을 저감하기 위하여 여러 가지 방법으로 연구가 진행되어 오고 있는데 그 중에 배기가스를 재순환하여 저감하는 방법이 있다. 본 연구는 배기가스를 재순환하는 방법으로 연소로 외부에 코안다 노즐을 이용하여 배기가스를 재순환 유입하는 방법을 사용하였다. 코안다 노즐을 이용하여 배기가스를 재순환하고 혼합가스는 연소로 접선 방향으로 투입하여 선회유동을 유발하는 특징을 가지는 배기가스 재순환 버너이다. 이러한 버너에서 연소로 내의 선회 유동 특성을 살펴보고 온도와 반응속도 분포를 살펴봄으로써 코안다 노즐을 이용한 재순환 버너의 연소 유동 특성을 규명하였다. 과잉공기계수와 코안다 노즐 간격을 변화하여 배기가스 재순환 유입량 특성을 살펴보았으며 과잉공기계수를 증가하면 재순환 유입량비가 증가하였고 코안다 노즐 간격을 증가하면 코안다 노즐 공기 출구에서 속도가 낮아져서 재순환 유입량이 감소한다는 특성을 알았다. 배기가스 출구에서 평균온도는 코안다 노즐 간격 변화에 거의 무관하며 과잉공기계수 증가에 따라 감소하는 것을 알았다. 이러한 특성으로 배기가스 출구에서 NOx 농도는 과잉공기계수 증가에 따라 현저히 감소하고 코안다 노즐 간격에는 상대적으로 영향이 적은 것으로 나타났다.

• 한국가시화정보학회지
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• 제1권2호
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• pp.29-37
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• 2003

During the past five decades or so, the characteristics of turbulent swirling flow have been studied extensively because of its great technological and scientific importance. It is well known that the swirling flow improves heat transfer in duct flow. The reason for this is due to the effect of streamline curvature associated with the tangential velocity component. Although many studies have been carried out to investigate the characteristics of the swirling flow in a circular tube. The experimental methods for measuring the velocity components are by hot-wire or LDV (Laser-Doppler-Velocimetry) measuring single point velocity so far. The present study was aimed to analyse the flow characteristics of swirling flow such as time-mean velocity vector, local velocity turbulence intensity and turbulence kinetic energy by using PIV(Particle-Image Velocimetry). The experiment was carried out for four Reynold numbers $1.0\times10^{4}$, $1.5\times10^{4}$, $2.0\times10^{4}$ and $2.5\times10^{4}$ of the measuring area.