• 한국화재소방학회논문지
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• 제33권3호
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• pp.37-43
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• 2019

본 연구에서는 2유체노즐을 이용하여 에탄올 풀화재(Ethanol pool fire) 소화 실험을 수행하였다. 화원 면적이 5.027 × 10^-3 ㎡와 1.131 × 10^-2 ㎡(연료팬 직경은 각각 80 mm와 120 mm)를 대상으로 하였고, 화재 소화 실험 시 2유체노즐로의 공급 유량의 경우 물은 156-483 g/min, 공기는 20-70 L/min 조건이었다. 화원 면적이 증가하면 열방출률도 증가하였고, 화원 면적이 5.027 × 10^-3 ㎡와 1.131 × 10^-2 ㎡일 때의 열방출률은 각각 1.01 kW와 5.51 kW로 측정되었다. 본 실험 영역에서 2가지 화원 면적 조건 모두, 물 공급 유량 조건과는 상관없이 공기 공급 유량이 40 L/min 이상의 조건에서 소화가 가능하였다. 소화 소요 시간 및 물 소모량의 경우 모든 물 공급 유량 조건에서 공기 공급 유량이 증가함에 따라 감소하는 경향이 관찰되었고, 공기 공급 유량이 비교적 많은 영역(예를 들면, 약 50 L/min 이상)에서 소화 소요 시간은 약 23 s, 물 소모량은 약 185 g 이내로 나타났다. 본 연구 결과와 단일유체노즐을 이용한 기존 연구 간 단위 열방출률 당 물 소모량 비교를 통하여, 2유체노즐이 단일유체노즐에 비해 더 적은 물 소모량으로 소화가 가능할 수 있음을 확인하였다.

• International Journal of Fluid Machinery and Systems
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• 제2권3호
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• pp.248-253
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• 2009

This paper presents a numerical study for unsteady flows in a high-pressure steam turbine with a partial admission stage. Compressible Navier-Stokes equations are solved by the high-order high-resolution finite-difference method based on the fourth-order compact MUSCL TVD scheme, Roe's approximate Riemann solver, and the LU-SGS scheme. The SST-model is also solved for evaluating the eddy-viscosity. The unsteady two-dimensional flows through whole nozzle-rotor cascade channels considering a partial admission are numerically investigated. 108 nozzle passages with two blockages and 60 rotor passages are simultaneously calculated. The influence of the flange in the nozzle box to the lift of rotors is predicted. Also the efficiency of the partial admission stage changing the number of blockages and the number of nozzles is parametrically predicted.

• 연구논문집
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• 통권25호
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• pp.47-54
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• 1995

The atomizing characteristics in a spray injected from a twin fluid atomization nozzle have been investigated. The Sauter mean diameters as mean diameter are compared with wavelength calculated from the instability theory. The Sauter mean diameter are measured by the Fraunhofer diffraction theory using the Malvern particle sizer. The wavelength is calculated using the mean relative velocity instead of the exit relative velocity of nozzle. Also shadowgraphy technique is used to visualize atomization. This paper gives a possibility that the mean diameter can be predicted with the wavelength obtained by the simple instability theory.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 1998년도 유체기계 연구개발 발표회 논문집
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• pp.27-32
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• 1998

This paper presents the development of a two-dimensional model for investigating the fluid flow in water jet and calculating the velocity and pressure distributions. The mathematical formulation as a standard k-$\epsilon$ model was solved employing a general thermofluid-mechanics computer program, PHOENICS code, which is based on the Semi-Implicit Method Pressure Linked Equations(SIMPLE) algorithm. The developed code was applied to water jet design to determine the nozzle size, and investigated the effect of the change of nozzle location. Calculated results showed that the flow pattern is not changed as the change of nozzle location.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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• pp.1048-1050
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• 2017

본 연구에는 핀틀 노즐의 열변형 영향을 평가하기 위해 단방향 유체-구조 연성해석을 수행하였다. 단방향 유체-구조 연성해석을 위해 핀틀-노즐의 내부에 발생하는 압력 및 온도분포를 유동해석을 통해 도출하였고, 압력 및 온도분포 값을 각각의 유체-구조 해석의 하중조건으로 적용하여 핀틀의 변형량을 확인하였다. 변형에 대한 추력특성 변화를 확인하기 위해 양방향 유체-구조 연성해석을 수행 중이다.

• International Journal of Fluid Machinery and Systems
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• 제6권4호
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• pp.206-212
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• 2013

Self-excited pulse jet is a specific nozzle with a closed chamber which can change a continuous jet into a pulse one. Energy of the pulse jet can be output not only unevenly but also with multifrequency. With the peak pressure of pulse jet, the hitting power would be 2~2.5 times higher than that of continuous jet. In order to reveal the correlation between the self-excited pulse frequency and nozzle diameter ratio, nozzle spacing and operating pressure, the model of 3D unsteady cavitation model has been used. We found that with the same nozzle structure parameters and the different operating pressure, the self-excited frequency and the width of peak crest are different, but the wave profiles are similar. With FFT, we also found that the less bandwidth of amplitude in low frequency range will lead to the wider wave crest of outlet velocity in its time domain, and the larger force of the strike will be gained. By studying the St of self-excite nozzle, not only the frequency of a certain nozzle can be predicted, but also a nozzle structure with a certain frequency can be designed.

• International Journal of Fluid Machinery and Systems
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• 제5권1호
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• pp.30-37
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• 2012

A two dimensional Darrieus-type turbine has been proposed for the hydropower utilization of extra-low head less than 2m. In a practical use of Darrieus-type hydro-turbine, head and flow rate may be varied temporally and seasonally. Considering that the cost advantage is required for the low head hydro turbine system, the Darrieus turbine should be operated with high efficiency in the wider range of flow rate possibly by using an additional device with simpler mechanism. In the present paper, an adjustment of inlet nozzle section by lowering the inlet nozzle height is proposed to obtain the preferable inlet velocity in low flow rate conditions. Effects of resulting spanwise partial inlet flow are investigated. Finally, an effective modification of inlet nozzle height over flow rate variation is shown.

• 한국유체기계학회 논문집
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• 제13권6호
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• pp.13-18
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• 2010

The programs of grid generation and flow analysis for the 3-D flow field. were developed. The finer results from numerical analysis could be obtained by using developed programs than those of the experimental data in the flow field of the circular nozzle exit region. Especially A virtual-origin of 3.2 times of nozzle diameter within three percent error inside from nozzle exit plane could be obtained.

• 한국분무공학회지
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• 제1권1호
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• pp.21-27
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• 1996

This experimental study was to investigate spray angles and drop sizes in an external mixed twin-fluid swirl jet nozzle. Twin-fluid swirl jet nozzle with swirlers designed four swirl angles such as $0^{\circ},\;22.5^{\circ},\;45^{\circ},\;64.2^{\circ}$ was employed. A PDA system was utilized for the measurement of drop size and mean velocity. Water and air were used as the working fluids in this experiment. The mass flow rate of water was fixed as 0.03 kg/min, and air flow rates were controlled to have the air/liquid mass ratio from 1.0 to 6.0. As a result, swirl angle controlled to spray angles and drop sizes. It was found that swirl angle was increased with spray angle and with decreased SMD. However, the effect of swirl angle was reduced at large air/liquid mass ratio(Mr=6.0).

• 대한환경공학회지
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• 제37권1호
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• pp.23-33
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• 2015

본 연구는 물탱크 내부의 사류구역 최소화에 목적을 두고 진행하였으며 입수관의 형태를 개선하여 물탱크 내부에서 발생하는 유동특성을 전산유체역학(Computational Fluid Dynamics, CFD)모사 기법을 이용하여 분석 하였다. 기존에 물탱크에 사용되던 자유낙하 방식의 입수관을 다공형 스크류 노즐 입수관으로 개선하고 유동 특성을 분석한 결과 노즐 안에 스크류 날개가 설치된 경우 유동흐름의 폭이 넓게 분사 되었으며 원통형 물탱크 내부에서도 넓은 유동 흐름이 나타났다. 또한 사각형 물탱크에 다공형 스크류 노즐 입수관이 1개 설치되어 있을 경우와 2개 설치되어있을 경우의 유동해석과 추적자모의를 수행하였으며 그 결과 입수관을 2개 설치할 경우 MODAL, MORILL index값이 1에 가깝게 나타나 Plug Flow 특성에 근접하단 결과를 얻을 수 있었다.