• 설비공학논문집
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• 제13권3호
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• pp.209-216
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• 2001

A numerical study is peformed to investigate the effect of circumferential velocity generated by the guide vane on the nozzle flow of a jet fan, s a way of increasing the penetration force of jet fan with nozzle of 175mm diameter. For the validation of numerical results. the velocity is measured by a 5-hole pitot tube and flow visualization is conducted by the tuft method. Under the inlet condition that the maximum circumferential velocity in the stator outlet of the present jet fan is 1.8m/s, the axial velocity in the nozzle outlet has the feature that the velocity at the axis is low and the velocity near the wall high. Therefore, to increase the throw length of the jet fan, the configuration of the fairing and nozzle needs to be developed and the precise revise of the stator angle is required, In addition, the bigger the circumferential velocity, the smaller the axial velocity at the axis and the bigger non-uniformity of the flow distribution.

• 한국자동차공학회논문집
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• 제4권4호
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• pp.72-79
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• 1996

The recent trend of higher output engines with more auxiliary parts is resulting in greater heat generation in the engine compartment. In order to maximize the heat dissipation and eliminate the inefficient flow in the engine compartment, it is necessary to understand the flow field under the hood. In this respect, experimental study as well as numerical analysis should be conducted. The automated measuring system was constructed to obtain three dimensional mean flow data with high accuracy. The measurements have been made on a vehicle with a steady incoming air flow. The result shows that there exists a high degree of non-uniformity in the mean flow velocity at the front of radiator.

• 대한토목학회논문집
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• 제29권4B호
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• pp.357-363
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• 2009

일반적으로 사용되는 관수로의 평균유속을 구하려면 Darcy-Weisbach의 마찰손실수두공식을 사용하면 되나, 그러나 이 식의 마찰손실계수 f는 Reynolds수와 상대조도(${\varepsilon}$/d)의 함수이므로 사용하기에 매우 불편하며 따라서 보다 편리한 식이 요구된다. 이에 본 연구에서 Chiu 유속공식의 신뢰성과 정확성을 증명하기 위하여 관수로에서 비삽입식 유속측정 장치인 레이저 유속계(Laser Doppler Velocimeter: LDV) 및 초음파 유량계(Ultrasonic Flowmeter: U/F), 삽입식 유속측정장치인 피토관 (Pitot Tube)을 이용하여 실측한 유속측정 자료와 Chiu의 공식을 이용한 유속분포가 매우 잘 일치함을 증명하였다. 유량의 증감에 관계없이 실험실 수로에서의 최대유속과 평균유속간의 이론적인 선형관계를 증명함으로써 관수로내 유속의 평형상태, 즉 엔트로피 파라미터 M값에 대응하는 평형상태에 도달하려 하고 이 평형상태를 지속적으로 유지하려고 하는 경향이 있음을 증명하였다. 또한, 한 단면을 대표하는 엔트로피 파라미터 M값이 결정되면 최대유속이 발생하는 지점에서의 유속 측정만으로 단면 전체의 평균유속을 쉽게 구할 수 있고 이로부터 간단히 유량을 산정할 수 있음을 증명하였으며, 이는 추후 관수로 설계 및 운영관리 시 가장 중요한 평균유량을 측정할 수 있는 이론적인 도구로 사용될 수 있음을 의미하는 것이다.

• 대한기계학회논문집
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• 제15권1호
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• pp.262-273
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• 1991

본 연구에서는 벽면에서의 압력은 압력측정 정치를 제작하여 측정하였으며 평 균유동 및 난류량들은 열선 유속계(hot wire system)을 사용하여 측정하였다.

• 대한기계학회논문집B
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• 제27권8호
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• pp.1061-1070
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• 2003

A triple flame in a mixing layer was studied experimentally with concentration gradient and mean velocity by using a multi-slot burner, which can stabilize the lift-off flame. Flame stabilization condition, lift-off heights, and some other characteristics were examined for methane and propane flame within a range of very low concentration gradient. Pitot-tube and LDV(Laser Doppler Velocimetry) were used for velocity. Mass spectroscopy and Rayleigh scattering signal were used for concentration gradients. Thermo-couples and SiC TFP(Thin Filament Pyrometer) were used for temperature. It was found that minimum values of the lift-off heights exist at a certain concentration gradient for constant mean velocity and this means that the propagation velocity has a maximum value. The scales of flame to the burner nozzle and intensity variation of the diffusion flame were suspected as the cause.

• 오토저널
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• 제12권3호
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• pp.53-62
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• 1990

A wind tunnel experiment for the flow around a 1/5 scale passenger vehicle model has been carried out. A 5-hole Pitot tube is used for measuring velocity distributions around the model and a scanivalve with 48 ports is used for measuring surface pressure distribution at various Reynolds numbers. In order to observe the flow on the surface and in the wake region, a flow visualization experiment has been performed using wool tuft with and without paper cones. In addition, a 2-dimensional viscous calculation considering only the mid-plane section of the model has been performed. A complex wake structure in the immediate rear of the model has been confirmed. The distributions of the surface pressure coefficient are not sensitively dependent on the Reynolds Number. In the first half of the model, they do not seem to vary form section to section. However, in the second half, they do vary from section to section, especially at the bottom surface, which indicates that the cross flow vortex is more affected by the bottom surface than the top surface. The qualitative agreement of the measured and calculated velocity field also explains the usefulness of the 2-dimensional calculation in the limited sense.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2005년도 춘계학술대회논문집
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• pp.170-175
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• 2005

The focus of this paper is to observe the aerodynamic and vibration characteristics of the NACA0012 blade(AR=16.6) fixed on the lower surface of the wind tunnel, by changing air speed and the blade's angle of attack. After fixing a slit-typed vortex generator on the front of the blade, it could be observed that the vibrational characteristics caused by interactions between vortex and blade through the 5-hole pilot tubes. And, also, two different blades in stiffness had been prepared for observing those characteristics above in this experiment. The results were compared with the given stiffness of blade, as well. According to the results, it is clear to recognize that the vibration spectrum increases while air speed and angle of attack increase, and, also, less stiffness means bigger vibration spectrum.

• 한국항공우주학회지
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• 제36권10호
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• pp.1017-1025
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• 2008

본 연구에서는 무인항공기의 대기속도 및 압력고도를 측정하는 공력자료시스템(ADS)을 개발하였다. ADS는 비행제어시스템에 항공기 속도와 고도를 제공함으로써 실속속도 이하에서의 비행을 막고 고도유지 비행을 가능하게 하는 시스템이다. 무인항공기의 속도와 고도를 정확하게 측정하는 것은 비행성능을 확인하고 항공기의 안전성을 보장하기 위한 중요한 부분이다. 본 논문에서 개발된 ADS는 MEMS 압력센서, 저역통과필터, 마이크로 컨트롤러 그리고 피토튜브로 구성되어 있다. 온도보정과 압력보정을 통해 ADS 데이터의 오차를 줄였으며 비행시험에서 GPS 데이터와 ADS 데이터를 비교하였다.

• 한국지열·수열에너지학회논문집
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• 제9권3호
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• pp.19-25
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• 2013

A new type axial flow fan with centrifugal sub-blades has been designed and fabricated in the present study. We investigated velocity and pressure distributions in downstream flow fields of the fan experimentally to detect the detailed flow characteristics of new axial flow fan and an existing axial flow fan. Two-dimensional velocity components were probed by applying a particle image velocimetry system and pressure distributions were measured by Pitot tube and micro-manometer. Our results show that the velocity and pressure distributions at the flow fields of the new fan are quite different from the existing fan, and that the centrifugal sub-blades in the new fan can improve the performance characteristics in view of kinetic energy.

• 대한기계학회논문집B
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• 제30권4호
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• pp.373-380
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• 2006

Annubar is one of popular tools to measure the exhausted gas flow rate from the stacks. For the accurate monitoring of the amount of discharged pollutants, calibration of annubar is very important. Calibration of annubar has been carried out in a wind tunnel. When the length of annubar is longer than the test section size of wind tunnel, it is very difficult to find out typical value of annubar coefficients. So, a measurement technique to calibrate annubar longer than the size of the test section of wind tunnel must be developed. In the present study, an experiment is performed to measure the annubar coefficients in such a limited size of the wind tunnel. The experimental annubar coefficient by using a partial blocking technique is very close to the annubar coefficient of normal condition.