• 한국분무공학회지
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• 제10권1호
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• pp.1-9
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• 2005

When the water jets heated up to the saturation temperature at a high line pressure are sprayed into a reduced (atmospheric) pressure through an air-assisted nozzle, the jets experience sudden exposure into a reduced pressure, get superheated and produce steam bubbles while atomization processes of jets are taking place. This process is called flash atomization. In this study the flash atomization of superheated water jets assisted by air has been studied. Sprays with flash atomization have been photographed at various water and air flow rates and water superheats. It has been found that the spray angle with flash atomization increases with water superheat and water flow rate but decreases with air flow rate. The degree of change of spray angle has been analyzed and correlated as a function of superheat, air and water flow rates.

• Computers and Concrete
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• 제2권2호
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• pp.97-110
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• 2005

Rheological behaviour of fresh concrete is an important factor in controlling concrete quality. It is recognized that the measurement of the slump is not a sufficient test method to adequately characterize the rheology of fresh concrete. To further understand the slump measurement and its relationship to the rheological properties, an elasto-viscoplastic, 2-D axisymmetric finite element (FE) model is developed. The FE model employs the Bingham material model to simulate the flow of a slump test. An experimental program is carried out using the Slump Rate Machine (SLRM_II) to evaluate the finite element simulation results. The simulated slump-versus-time curves are found to be in good agreement with the measured data. A sensitivity study is performed to evaluate the effects of yield stress, plastic viscosity and cone withdrawal rate on the measured flow curve using the FE model. The results demonstrate that the computed yield stress compares well with reported experimental data. The flow behaviour is shown to be influenced by the yield stress, plastic viscosity and the cone withdrawal rate. Further, it is found that the value of the apparent plastic viscosity is different from the true viscosity, with the difference depending on the cone withdrawal rate. It is also confirmed that the value of the final slump is most influenced by the yield stress.

• 한국전산유체공학회지
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• 제17권3호
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• pp.18-24
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• 2012

The aerodynamic performance of the pantograph on a high speed train was compared for different pantograph covers which are designed to block the aero-acoustic noise from the pantograph. For the study, two types of cover are designed: wedge and cone types. The lift force of pantograph with cover was compared with the force of pantograph only. The comparison clarified that the cone type cover increases the sideslip angle of the flow and decreases the lift force considerably. However, the wedge type cover changes the flow direction upward and increases the lift force of the pan head. This increment of lift force compensates the decrement of lift force caused by the blocking of the flow into the pantograph lower frame due to cover. Therefore, in case of the wedge type cover, the overall lift force changes slightly compared with the cone type cover.

• 설비공학논문집
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• 제9권1호
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• pp.55-63
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• 1997

A numerical investigation has been made for flows in an axisymmetric circular cylinder with an impulsively rotating cone located at the bottom of the container. The axisymmetric container is completely filled with a viscous fluid. Major parameter for the present research is only the vertex angle of the cone, otherwise Reynolds number and aspect ratio of the vessel are fixed. Main interest concerns on the vortex breakdown of meridional circulation by impulsive rotation of the cone with respect to the longitudinal axis of the cylinder. Numerical method has been used to integrate momentum and continuity equations on a generalized body-fitted grid system. The pattern of vortex breakdown is quite different from that in a right circular cylinder with flat endwall disks. The flow visualization photograph of the preceeding work by Escudier is compared with the present numerical results and the two results are in good agreements. Also flow data are plotted to gain a deep understanding for the present phenomena of the vortex breakdown. The conclusions of this work are clearly explained by the classical theory of the vortex flows in a finite geometry.

• 한국항공우주학회지
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• 제31권7호
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• pp.26-31
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• 2003

수직 이착륙기나 로켓 등을 발사시킬 때 사용되는 제트 편향기 설계를 위한 기초 자료를 얻기 위해 축대칭 원뿔에 충돌하는 초음속 제트에 대한 연구를 수행하였다. 본 논문에서는 충격파 간섭 또는 전단층에 의한 박리 등과 같은 유동 현상을 분석하기 위해 쉬리렌 장치를 이용한 유동가시화, 표면압력분포 등을 측정하였으며, 수치해석을 통해 실험결과와 비교, 검증하였다. 유동은 원뿔 충격파와 배럴 충격파 사이에서 간섭으로 인해 발생되는 충격파 패턴이었으며, 자유제트의 구조에 따라 다양한 형상을 나타내며 표면 압력분포에 크게 영향을 미친다.

• 한국화재소방학회논문지
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• 제34권3호
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• pp.28-34
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• 2020

고체 가연물 주위의 유동과 열적 두께의 변화가 열방출률 특성에 미치는 영향을 고찰해보기 위해 ISO 5660-1 콘 칼로리미터 실험을 수행하였다. 고체 가연물로는 연소반응 중 Char를 발생시키지 않는 Polymethyl methacrylate (PMMA)를 선정하였고 열침투깊이를 계산하여 PMMA의 열적 두께를 구분하였다. 콘 칼로리미터의 덕트 유동을 12, 24, 40 L/s로 설정하여 가연물 주위에 강제 유동을 발생시킨 뒤 PMMA의 연소 시 측정된 열방출률을 측정함으로써 열분해 특성을 분석하였다. 열적으로 얇은 가연물의 열방출률은 주위의 유동 변화에 크게 영향을 받지 않았지만, 열적으로 두꺼운 가연물은 유량의 변화에 따라 열방출률이 크게 영향 받는 것을 확인하였다.

• 대한기계학회논문집B
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• 제21권5호
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• pp.637-649
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• 1997

Effects of cone angle, pressure-hole orientation and Reynolds number on the five-hole probe calibration have been investigated for eight large-scale conical five-hole probes, which have either perpendicular pressure holes or forward-facing pressure holes for the cone angles of 45 deg, 60 deg, 75 deg and 90.deg. Pitch and yaw angles are changed from -40 deg to +40 deg with an interval of 5 deg, respectively, when the probe Reynolds numbers are 1.77*10$^{4}$, 3.53*10$^{4}$ and 7.06*10$^{4}$. The result shows that larger cone angle results in more sensitive changes in the calibration coefficients. In the case that the cone angle is 45 deg, the pitch-angle and yaw-angle coefficients of the five-hole probe with the perpendicular pressure holes show a very different trend compared with those of the five-hole probe with the forward-facing pressure holes. On the other hand, when the cone angle is more than 60 deg, each calibration coefficient is nearly independent of the pressure-hole orientation. Additionally, the effects of the Reynolds number on the calibration coefficients are also reported in detail.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2011년도 제36회 춘계학술대회논문집
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• pp.57-60
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• 2011

GCSC 분사기의 리세스 길이와 기체/액체의 운동량 플럭스 비(MFR) 변화에 따른 분무 특성을 고압 챔버를 이용한 고압수류시험을 통해 알아보았다. 물과 질소를 사용하였고, back-lit strobe imaging 기법을 이용하여 분무형상을 촬영하였다. 시험결과 MFR이 작을 때(액체 유속 고정)는 분무각이 큰 hollow cone 형상을 보이고, MFR이 증가함에 따라 분무각이 작은 solid cone 형상의 분무를 보였다. 또한 리세스가 짧은 분사기일수록 더 큰 MFR에서 solid cone 형상의 분무를 보였다.

• 한국전산유체공학회지
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• 제13권2호
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• pp.8-13
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• 2008

A supersonic viscous flow over a five-degree half-angle cone is studied computationally with three-dimensional Navier-Stokes equations. Steady asymmetric solutions show that the asymmetric flow separation is caused by convective instability. The effects of angle of attacks, Reynolds numbers, and Mach numbers have been investigated and it is found that those factors affect the generation of the side force. The side force has the maximum value at ${\alpha}=22^{\circ}$, while over ${\alpha}=22^{\circ}$, asymmetric vortex becomes transient, which results in the unsteady shedding. At the angle of attack of 22 degrees, the side force increases with Reynolds number and decreases with Mach number. The increase of the side force stops over the critical Reynolds number for the present configuration.

• 한국항공운항학회지
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• 제14권1호
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• pp.43-48
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• 2006

The present study was carried out in order to develope a seven-hole pressure probe which is able to measure high flow angles. The seven-hole pressure probe is a non-nulling, directional velocity probe used for measuring three dimensional flow that having high flow angles. A 4 mm diameter seven-hole conical pressure probe was manufactured with a cone angle of 70$^{\circ}$. The probe was comprised of seven 1 mm diameter stainless steel tubes packed close together and fitted into an outer stainless steel sleeve. The calibration procedure is based on the use of the Callington's polynomial curve-fit method. The validity of the seven-hole conical pressure probe is demonstrated by comparisons with hot-wire data.