• 한국항공운항학회지
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• 제14권2호
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• pp.33-38
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• 2006

Heat transfer coefficients and static pressure distributions on a gas turbine vane endwall were experimentally investigated in a 5 bladed linear cascade. The Reynolds number based on an axial chord length and the cascade exit velocity was 500,000. Both heat transfer and pressure measurements on the vane endwall were made at the two different turbulence intensity levels of 6.8% and 10.8%. Detailed heat transfer coefficient distributions on the vane endwall region were measured using a hue detection based transient liquid crystals technique. Results show various regions of high and low heat transfer coefficients on the vane endwall surface due to several types of secondary flows and vortices. Heat transfer coefficient and endwall static pressure distributions showed similar trends for both turbulence intensity, however, the averaged heat transfer coefficients for higher turbulence intensity case was higher than the lower turbulence intensity case by 15%.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2006년 제4회 한국유체공학학술대회 논문집
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• pp.187-190
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• 2006

In the present study, effects of tree-stream turbulence and surface trip wire on the flow past a sphere at $Re\;=\;0.4\;{\times}\;10^5\;{\sim}\;2.8\;{\times}\;10^5$ are investigated through wind tunnel experiments. Various types of grids are installed upstream of the sphere in order to change the tree-stream turbulence intensity. In the case of surface trip wire, 0.5mm and 2mm trip wires are attached from $20^{\circ}\;{\sim}\;90^{\circ}$ at $10^{\circ}$ interval along the streamwise direction. To investigate the flow around a sphere, drag measurement using a load cell, surface-pressure measurement, surface visualization using oil-flow pattern and near-wall velocity measurement using an I-type hot-wire probe are conducted. In the variation of free-stream turbulence, the critical Reynolds number decreases and drag crisis occurs earlier with increasing turbulence intensity. With increasing Reynolds number, the laminar separation point moves downstream, but the reattachment point after laminar separation and the main separation point are fixed, resulting in constant drag coefficient at each free-stream turbulence intensity. At the supercritical regime, as Reynolds number is further increased, the separation bubble is regressed but the reattachment and the main separation points are fixed. In the case of surface trip wire directly disturbing the boundary layer flow, the critical Reynolds number decreases further with trip wire located more downstream. However, the drag coefficient after drag crisis remains constant irrespective of the trip location.

• 제어로봇시스템학회논문지
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• 제14권4호
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• pp.336-341
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• 2008

Recently, research on a flat panel display(FPD) has focused on organic light-emitting display(OLED) which has wide angle of view, high contrast ratio and low power consumption. ITO(Indium-Tin-Oxide) films are the most widely used material as a transparent electrode of OLED and also in many other display devices like LCD or PDP. The performance and efficiency of OLED is related to the surface condition of ITO coated glass substrate. The typical surface defect of glass substrate is measured for electric characteristics and physical condition for transmittance and roughness. Since ITO coated glass substrate can be destroyed for inspection about surface roughness, sheet resistance, film thickness and transmittance, precise fabrication condition should be made based on the estimated relationship. In this paper, ITO films were prepared on the commercial glass substrate by the Ion-Plating method changing the partial pressure of gas(Ar, 02) and the chamber temperature between $200^{\circ}C$ and $300^{\circ}C$. The characteristics of films were examined by the 4-point probe, supersonic thickness measurement, transmittance measurement and AFM. We estimated the relationship between processing parameters(Ar gas, O2 gas, Temperature) and properties of ITO films (Sheet Resistance, Film Thickness, Transmittance, Surface Roughness).

• 터널과지하공간
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• 제22권1호
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• pp.54-59
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• 2012

노천에서 폭파실험을 통해 납판 발파압계의 변형량을 계측하였다. 홉킨슨 바 시험장치의 가스 건으로 압력 실험하여 구한 보정 그래프에 계측데이터를 적용하여 폭풍압을 산출하였다. 그 결과를 CONWEP, DDESB 등 여러 가지 폭풍압 예측식과 대비하였다. 근거리 폭풍압의 실 계측 값은 폭풍압 예측식의 결과보다 최대압력이 낮게 나타났지만 거리에 따른 압력감쇠는 폭풍압 예측식보다 완만한 것을 확인할 수 있었다. 이는 기존 이론식으로 추정한 초근접 지점의 발파압은 부정확함을 의미한다.

• Journal of Mechanical Science and Technology
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• 제16권9호
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• pp.1121-1136
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• 2002

The flow characteristics of film coolant issuing into turbulent boundary layer developing on a convex surface have been investigated by means of flow visualization and three-dimensional velocity measurement. The Schlieren optical system with a spark light source was adopted to visualize the jet trajectory injected at 35° and 90° inclination angles. A five-hole directional pressure probe was used to measure three-dimensional mean velocity components at the injection angle of 35°. Flow visualization shows that at the 90° injection, the jet flow is greatly changed near the jet exit due to strong interaction with the crossflow. On the other hand, the balance between radial pressure gradient and centrifugal force plays an important role to govern the jet flow at the 35° injection. The velocity measurement shows that at a velocity ratio of 0.5, the curvature stabilizes downstream flow, which results in weakening of the bound vortex structure. However, the injectant flow is separated from the convex wall gradually, and the bound vortex maintains its structure far downstream at a velocity ratio of 1.98 with two pairs of counter rotating vortices.

• 한국가시화정보학회지
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• 제13권3호
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• pp.29-34
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• 2015

The interaction between a normal shock wave and a boundary layer along a wall surface in internal compressible flows causes a very complicated flow. This interaction region containing shock train and mixing region is called as pseudo-shock waves. Pseudo-shock waves in the divergent part of a rectangular nozzle have been investigated by using large-eddy simulation (LES). LES studies have been done for the complex flow phenomena of three-dimensional pseudo-shock waves. The LES results have been validated against experimental wall-pressure measurements. The LES results are in good agreement with experimental results. Pseudo-shock length and corner separation have been studied in three-dimensional LES model. Comparison of centerline pressure measurement and 3D visualization measurement has been discussed for the corner separation position. It has been concluded that the pseudo-shock length should be measured by using 3D visualization measurement.

• 터널과지하공간
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• 제5권4호
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• pp.347-362
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• 1995

The purpose of this study was that manage effectively the excavation process of the transport tunnel in DONGHAE mine area by investigating the variationof the surface and groundwater flow system around the tunnel and neighbouring villages. Thus, the effect of excavation and water-prrofing process on the water system has been studied through the naked eye survey of the tunnel and the surface outcrop, joint survey, core drilling, the measurement of the surface water quantity, evapotranspiration and precipitation analysis, rock hydraulics approach, the pressure test of boreholes, the variation of the water level, and finally the numerical analysis. From above approachs, we derived the conclusion that the exhaustion of the surface water was not caused by the tunnel excavation on the groundwater system was minimized by effective water proofing process.

• 한국압력기기공학회 논문집
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• 제19권2호
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• pp.155-162
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• 2023

In nuclear power plants, the flow rate information is a major indicator of the performance of rotating equipment such as pumps, and is a very important one required for facility operation and maintenance. To measure a flow rate, various types of methods have been developed and used. Among them, the differential pressure type using orifice and the direct doppler type using ultrasonic waves are the most commonly used. However, these flow rate measurement methods have limitations in installation, conditions and status of the measuring part, etc. To solve this problem, we have studied a new technique for measuring flow rate from scratch. In this paper, we have devised a technique to estimate the flow rate using an average moving velocity of large-scale eddy in turbulence that occurs in the piping flow field. The velocity of the large-scale eddy can be measured using the pressure fluctuation signals on the inner surface of the pipe. To estimate the flow rate, at first a cross-correlation function is applied to the two pressure fluctuation signals located at different positions in the down stream for calculating the time delay between the moving eddies. In order to validate the proposed flow rate estimation method, CFD analyses for the internal turbulence flow in pipe are conducted with a fixed flow condition, where the pressure fluctuation signals on the pipe inner surface are simulated. And then the average flow velocity of the large scale eddy is to be estimated. The estimated flow velocity is turned out to be similar to the fixed (known) flow rate.

• 비파괴검사학회지
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• 제22권4호
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• pp.393-401
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• 2002

원자력 발전소나 화학공장 등에서 사용되는 보편적인 부재중 하나인 압력배관은 사용중에 내부에 부식 등의 원인으로 결함이 발생되어 구조적 강도나 안전에 문제를 야기한다. 따라서, 이런 결함의 검출은 중요한 문제이다. 현재 신뢰성이 인정되어 사용되는 기존의 비파괴검사법으로는 초음파 X선 그리고 와전류에 의한 방법 등이 있다. 그렇지만 이러한 방법들은 검사하고자 하는 대상과 거의 접촉에 가까운 형태로 검사가 진행되고 있으며, 결함은 넓은 영역에 걸쳐 한번에 검출되지 못하고 탐촉자나 필름이 위치하는 부분으로 검사영역이 한정되는 단점이 있다. 그래서 검사에 많은 시간과 경비가 소모되고 있다. 본 연구에서는 이러한 단점들을 극복할 수 있는 레이저를 이용한 전자 전단 간섭법으로 결함을 측정하였다. 그리하여 압력용기의 내부에 존재하는 다양한 결함의 유무와 결함의 방향을 변위구배를 나타내는 간섭무늬로 검출하고, 검출된 결함에 위상 이동법을 적용하여 정량적으로 측정할 수 있었다. 본 연구는 두 편으로 구성된다. 그 첫 번째는 전자 전단 간섭법을 이용한 압력용기의 내부결함 검출에 관한 연구이고, 두 번째는 그 측정시스템의 오차분석에 관한 연구로 구성되어 있다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2007년도 제28회 춘계학술대회논문집
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• pp.317-321
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• 2007

PSP는 Pressure Sensitive Paint의 약자로 대기중의 산소량을 측정하여 전역적인 압력정보를 광학적으로 측정 할 수 있다. 본 연구에서는 PSP를 사용하여 jet injection 후류의 표면압력 분포를 알아보았다. 또한 Jet injection 5mm앞에 종횡비 1에서 4까지의 사각형 Cavity를 위치시켜 후류에 미치는 영향을 알아보았다. Jet injection 후류의 압력 분포는 Cavity의 전단층의 영향으로 Cavity가 없을 때와 비교해서 옆으로 넓게 퍼지면서 강도는 약해지는 모습을 보인다. 또한 Cavity의 종횡비가 커짐에 따라서 전단층의 크기가 커지고 그 영향이 커졌다. 측정된 압력은 압력공의 결과, CFD의 결과와 비교하였으며 근접한 값을 보였다.