• Journal of Advanced Marine Engineering and Technology
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• 제22권5호
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• pp.643-651
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• 1998

Turbulent unsteady flows in the entrance region of a square duct are investigated with a hot-wire anemometer system. The velocity waveforms the mean and turbulence components of the axial velocity and the entrance length are obtained as a major characteristics of the developing turbulent unsteady flows. An inviscid flow theory is presented to describe the developing axial mean velocity profiles. A good agreement is seen between the measured and theoretically predicted values. The propagation of turbulence generated near the entrance of the square duct is satisfactorily approximated by an empirical correlation of the propagation of turbulence proposed so far. The local turbulence intensi-ty is found to be a little smaller in the accelerating phase than in the decelerating phase. The entrance length is about 60 times as large the hydraulic diameter.

• 대한기계학회논문집
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• 제12권4호
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• pp.900-915
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• 1988

본 연구에서는 주유동 방향이 알려진 3차원 난류유동에서 열선유속계의 경사 형 프로브와 Ⅰ형 프로브를 회전시키므로써 3방향 속도성분과 6방향 레이놀즈 응력을 비교적 간편하고 정확히 측정하는 방법을 고안하여 사용하였다.

• 한국축산시설환경학회지
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• 제16권1호
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• pp.41-50
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• 2010

본 연구 국내 여건에 적합한 돈사시설과 분뇨처리가 일체형으로 조합된 고상식 돈사를 개발하는데 있어 1차적으로 적합한 환기 시스템 선발을 하고자 수행하였다. 고상식 돈사는 가로 29m, 세로 9m, 높이 7.5m 이며, l층 높이는 3.1m, 2층 높이는 2.4m 설계 건축하였다. 각 처리별 환기시스템은 l층으로 부터 2층 중천장까지 처리별로 칸막이를 고상식 돈사 내에 설치하였다. 각 처리별 환기방식은 덕트입기$\rightarrow$측벽배기 (처리 V1), 처마입기 (측벽 천장)$\rightarrow$측벽배기 (처리 V2), 천장입기$\rightarrow$측벽배기 (처리 V3) 3개 환기방식을 조사하였다. 공기흐름도와 공기유속을 조사하였다. 공기유속 조사시 환기량은 최소, 중간, 최대로 설정하였다. 그 결과는 다음과 같다. 덕트입기에서 공기흐름도는 2층과 l 층에서 비교적 균일한 수직 하강흐름을 보였고, 처마입기 (측벽천장)는 2층과 1층에서 대칭의 공기유동 하강흐름을 보였다. 천장입기는 중천장을 따라 공기가 우산형태로 퍼지면서 배출되고 느린 공기유속 보이며 l층으로 하강흐름을 보였다 최소환기량일때 하부지점 (돈방 바닥으로부터 80 cm)의 공기유속은 덕트입기, 처마입기 그리고 천장입기 비슷한 경향이었다. 최대환기량일때 덕트입기에서 하부지점의 공기유속이 (0.10~0.26 m/s)로 변화폭이 적었고, 처마입기에서는 공기유속은(0.12~0.63 m/s)로 변화의 폭이 넓고, 천장엽 기는 공기유속이 (0.07~0.15 m/s)로 느리며 변화폭이 적었다. 이상의 결과 덕트입기를 고상식돈사에서 적용이 가능할 것으로 사료되나, 돼지 사양과 실증시험으로 좀 더 검증이 필요할 것으로 판단된다.

• 한국유체기계학회 논문집
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• 제4권4호
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• pp.37-42
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• 2001

In the present study, flow characteristics of turbulent oscillatory flow in an oscillator connected to square-sectional $180^{\circ}$ curved duct are investigated experimentally. In order to investigate wall shear stress and pressure distributions, the experimental studies for air flows we conducted in a square-sectional $180^{\circ}$ curved duct by using the LDV system with the data acquisitions and the processing system. The wall shear stress at bend angle of the $150^{\circ}$ and pressure distribution of the inlet (${\phi}=0^{\circ}$) to the outlet (${\phi}=180^{\circ}$) by $10^{\circ}$ intervals of the duct are measured. The results obtained from the experiment are summarized as follows : wall shear stress values in the inner wall we larger than those in an outer wall, except for the phase angle (${\omega}t/{\pi}/6$) of 3, because of the intensity of secondary flow. The pressure distributions are the largest in accelerating and decelerating regions at the bend angle(${\phi}$) of $90^{\circ}$ and pressure difference of inner and outer walls is the largest before and after the ${\phi}=90^{\circ}$.

• 대한기계학회논문집
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• 제14권3호
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• pp.734-746
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• 1990

본 연구에서는 문등이 제안한 방법에 의하여 직사각형 단면의 180˚곡관유동 에서 속도분포와 난류성분을 측정하여 단면의 종횡비 변화에 따른 유동특성과 난류특 성의 변화를 고찰하였다.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2006년 제4회 한국유체공학학술대회 논문집
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• pp.213-216
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• 2006

This paper was a study about noise reduction through flow stabilization in duct using experimental method and numerical analysis at the same time. To determine the fan's type three kinds of fans(axial fan, centrifugal fan, and axial fan with centrifugal type blades) was examined to investigate the suitability for in-line duct. As a result, under the equal number of rotation 2000 RPM, performance of an axial fan with centrifugal type blades was the most superior by 55dBA at 4.3CMM among other fans. After this, analyzed the results of the numerical analysis to find out the optimum design of pitch angle such as $0^{\circ}$, $10^{\circ}$, $15^{\circ}$ and $20^{\circ}$. The intensity of turbulence was low when pitch angle was $15^{\circ}$ and air volume became peak by 5.08 CMM. It was observed that axis component of velocity increased gradually when pitch angle increased from $0^{\circ}$ to $20^{\circ}$, and embodied noise reduction and improvement of air flow rate through flow stabilization.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2004년도 추계학술대회
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• pp.1104-1109
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• 2004

The present study has been conducted to investigate convective heat/mass transfer inside the cooling passage with bleed holes. The rotating square channel has 40.0 mm hydraulic diameter and the bleed holes on the leading surface of the channel. The hole diameter of bleed hole is 4.5 mm and its spacing (P/d=4.9) is about five times of hole diameter. Mass flow rate through bleed holes is 10% of the main flow rate and rotation number is changed form 0.0 to 0.4. A naphthalene sublimation technique is employed to determine the detailed local heat transfer coefficients using the heat and mass transfer analogy. The cooling performance is influenced by mass flow rate through bleed holes and Coriolis force of rotating channel for fixed reynolds number. The heat transfer is enhanced around holes on the leading surface because of trapping flow by bleeding. However heat transfer on the leading surface is decreased due to Coriolis force.

• 설비공학논문집
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• 제2권3호
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• pp.188-198
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• 1990

Turbulent characteristics of turbulent pulsating flows were studied experimentally in a square duct. Velocity waveforms, velocity profiles, and turbulent intensity of turbulent pulsating flow were investigated by using a hot-wire anemometer with data acquisition and a processing system in a square duct with a ratio of 1 ($40mm{\times}40mm$) to 4,000mm long. Turbulent components were shown to be larger in decelerating than in accelerating regions and also larger for a large phase of velocity and U'rms distribution of turbulent flow. The effect of velocity amplitude ratio does not exist for specified time [${\theta}(z^{\prime})$], amplitude ratio (${\mid}U^{\prime}_{rms.os.1}{\mid}/{\mid}U_{m.os.1}{\mid}$), and phase difference (${\Delta}U^{\prime}_{rms.os.1}-{\Delta}U_{m.os.1}$) in either turbulent oscillating or cross-sectional mean velocity components. The effect of dimensionless angular frequency for specified time [${\theta}(z^{\prime})$] can be disregarded because the dimensionless angular frequency does not affect the specified time. The velocity distributions of turbulent pulsating flows for various time-averaged Reynolds numbers are in approximate agreement with the velocity distributions for equivalent Reynolds numbers and 1/7th power law of steady flow.

• 한국유체기계학회 논문집
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• 제17권5호
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• pp.19-26
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• 2014

The cross flow turbine attracts more and more attention for its relatively wide operating range and simple structure. In this study, a novel type of micro cross flow turbine is developed for application to a step in an irrigational channel. The head of the turbine is only H=4.3m and the turbine inlet channel is open ducted type, which has barely been studied. The efficiency of the turbine with inlet open duct channel is relatively low. Therefore, a guide nozzle on the turbine inlet is attached to improve the performance of the turbine. The guide nozzle shapes are investigated to find the best shape for the turbine. The guide nozzle plays an important role on directing flow at the runner entry, and it also decreases the negative torque loss by reducing the pressure difference in Region 1. There is 12.5% of efficiency improvement by attaching a well shaped guide nozzle on the turbine inlet.

• Journal of Biosystems Engineering
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• 제18권3호
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• pp.275-287
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• 1993

The flow characteristics of the transitional oscillatory flows are investigated analytically and experimentally in the entrance region of a square duct. The systems of conservation equations are analytically solved by linearizing the non-linear convective terms for the developing transitional oscillatory flows in a square duct. The analytical solutions are obtained in the form of infinite series for the velocity profiles. The experimental study for the air flow in a square duct is carried out to measure the velocity profiles and waveforms by using a hot-wire anemometer with the data acquisition and processing systems. The theoretical and experimental results provide the major characteristics of the developing transitional oscillatory flows, such as velocity profiles, velocity waveforms, and entrance length. The velocity profiles in the decelerating phase are larger than those in the accelerating phase for the developing transitional oscillatory flows. The correlations of the entrance length of the transitional oscillatory flows in a square duct are found to be $Le/Dh=K{\cdot}Re_{os}/2({\omega}^+)^2$, where K is 1.23 of an experimental constant.