• 대한조선학회논문집
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• 제49권2호
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• pp.203-211
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• 2012

The main object of this experiment is to estimate the hydrodynamic forces acting on a submerged streamlined body placed in a one-end-opened cylindrical tube moving with certain translational velocity. The best experimental design for this object is mimicking real situation, however sizes of model body and cylinder tube are just the same as those of real, for avoiding scale effects, mimicking real situation is not realizable. Hence, in this experiment, target body and cylindrical tube were designed to be towed with varying body position relative to cylindrical tube. For measuring hydrodynamic forces and flow velocity in the cylindrical tube, six one-component load cells and several one-hole Pitot tubes were used. Several conditions were checked with various end-plates those had different opening areas. Experiment results show that forces and flow velocity had different tendency with those expected, and the presence of a end-plate slows down the flow velocity in the cylindrical tube and affects pressure field in the tube to push the model submerged body forward of the tube. This tendency grows with decreasing opened area.

• 대한조선학회논문집
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• 제34권2호
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• pp.11-19
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• 1997

선미 반류분포를 계측하기위해 수조에서 흔히 사용하는 5공 피토관의 새로운 캘리브레이션 방법을 제안하였다. 기존의 한 각도(수평 또는 수직)만을 고려하는 1차원 캘리브레이션 방법과는 달리, 본 논문에서 제안한 2차원 차트 캘리브레이션 방법은 수평각과 수직각을 동시에 변화시켜 얻어진 2차원 차트를 이용하여 종전에 큰 각도에서 발생하던 오차를 줄임으로써 계측 정도를 크게 향상시켰다. 또한 종래의 1차원 방법에 맞추어 구성된 계측 시스템을 수정 없이 사용할 수 있도록 상관계수를 정의함으로써 사용의 편의를 도모하였다.

• 대한기계학회논문집B
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• 제23권5호
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• pp.646-652
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• 1999

Detailed characteristics of the mean flow field inside the rotor of a multiblade fan with scroll are presented in this paper by measurements and visualizations. The measurements were taken with a five-hole probe and conformed by smoke test. How field is distinguished clearly in 3 regions with respect to the flow directions. The first region is near the exit of scroll where the fluid flows the opposite direction to the rotation of rotor. The second is opposite side of the scroll exit where the fluid flows the same direction to the rotation of rotor. The third is the region where the fluid flows toward the blades directly with the largest values comparatively. The strongest recirculation is happened in the second region, and the weakest one is in the third region. This complex configuration makes the flow field highly non-uniform and may cause to generate a noise and ineffective flow efficiency.

• 대한조선학회논문집
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• 제51권4호
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• pp.311-320
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• 2014

Test uncertainty of a towed underwater Stereoscopic Particle Image Velocimetry (SPIV) system was assessed in a towing tank. To estimate the systematic error and random error of mean velocity and turbulence properties measurement, velocity field of uniform flow was measured. Total uncertainty of the axial component of mean velocity was 1.45% of the uniform flow speed and total uncertainty of turbulence properties was 3.03%. Besides, variation of particle displacement was applied to identify the change of error distribution. In results for variation of particle displacement, the error rapidly increases with particle movement under one pixel. In addition, a nominal wake of a model ship was measured and compared with existing experimental data by five-hole Pitot tubes, Pitot-static tube, and hot wire anemometer. For mean velocity, small local vortex was identified with high spatial resolution of SPIV, but has serious disagreement in local maxima of turbulence properties due to limited sampling rate.

• 설비공학논문집
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• 제9권1호
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• pp.14-22
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• 1997

The position of propeller fan from duct inlet is one of basic parameters for the design of propeller fan. To investigate the effect of its position on fan characteristics, the inlet flow fields and relative flow angles were measured by a 5-hole pitot tube. The experimental results indicate that the ratio of radial flow introduced from propeller circumference to total inlet flow increases with the increase of propeller distance from duct inlet. When fan operates without duct, the total flow rate and the radial flow ratio are higher than those of any other positions of propeller relative to duct inlet. The radial flow ratio decreases as a flow coefficient and the propeller distance decrease. Therefore the front flow fields can be adjusted in some extent by varying the propeller distance according to a fan loading. The inlet flow angles are decreasing a little as a rotational speed and the propeller distance decrease. In the present case it was judged that the deviation angle of outlet flow became negative owing to a flow separation near a trailing edge.

• 항공우주기술
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• 제7권2호
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• pp.46-52
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• 2008

5MW급 발전용 가스터빈의 주요 구성품 중 압축기에서의 성능시험 및 해석을 위해 측정 파라미터와 그 파라미터를 계측하기 위한 센서류를 선정하고자 한다. 축류압축기의 경우 각 단의 케이싱에서 정압 분포를 평균하여 계측하고, 내부 유동장에서 Kiel 온도관을 이용하여 전압 및 전온도 분포를 계측한다. 원심압축기의 경우 임펠러 출구의 허브면과 팁면에서의 정압 분포는 일반적으로 상당한 차이가 존재하므로 각 면에서 정압을 측정하여 평균하고, 디퓨저 내부와 디스월러 내부에서의 정압 분포를 계측하기 위해 한 피치에서 5개의 유선을 따라 10 곳에서 정압을 측정하고자 한다. 또한 압축기 내 유동특성과 동익-정익간의 상호작용을 고찰하기 위해 5공 피토관을 이용하여 내부 상세유동을 계측한다.