• Journal of Korea Water Resources Association
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• v.37 no.9
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• pp.781-787
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• 2004

The variation of channel bed which shows the complex hydraulic characteristics at channel junction was investigated by variation of discharge ratio and location of pier. As discharge ratio increase, the depth and width of erosion region become bigger to point of 63% of channel width in case of 1:0.5 discharge ratio. It was observed that the maximum scour depth at the point of 0.5 times of the channel width in the channel junction as 2.5 times bigger than straight channel. It means that the maximum scour depth at the channel junction is 2 times greater than by experimental formulas which are widely used in practical engineering, location of pier should be determined when it is installed in channel junction.

• Journal of Korea Water Resources Association
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• v.37 no.8
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• pp.623-630
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• 2004

In this paper, the hydraulic model tests are conducted for the hydraulic characteristics at channel junctions. The experiments are examined through the variation of approaching angle, discharge in the upstream main channel and the discharge ratio between the main channel and the tributary. The experiments are conducted in the channel model having the length of 450cm, the widths of 40cm and 32cm. Four water tanks and pumps are installed in the experimental channel. The length of stagnation zone is increased by Increasing of approaching angle and the discharge in the upstream channel. The length of stagnation increase with the discharge ratio between the main channel and the tributary. However, the variation of the stagnation zone near the channel junctions is little at the same approaching angles and the discharge ratioes between the main channel and tributary. However, the variation of the stagnation zone near the channel junctions is little at the same approaching angles and the discharge ratioes between the main channel and tributary. Accelerating zone of the velocity is occurred in the middle of the channel in the small approaching angle. However, the influence zone of the accelerating velocity is increased by increasing the approaching angle.

• Journal of the Korean Society of Propulsion Engineers
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• v.24 no.6
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• pp.61-68
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• 2020

7-tonf turbopump real-propellant tests in Naro Space Center were conducted and high-frequency signals from an accelerometer and pressure sensors installed on the casing and the inlet/outlet pipeline of LOX pump were analyzed to estimate the structural and hydrodynamic stabilities. Waterfalls, frequency spectrums and RMS(Root Mean Square) values of the measured signals were calculated and characteristic instability frequencies by the rotating cavitation and the rear floating ring seal(F.R.S) were investigated. Static pressures of the inlet/outlet pipeline and an acceleration of the pump casing are strongly affected on pressure fluctuation induced by the rear floating ring seal in the leakage path. Despite the acceleration RMS value seems totally small, the rotating-speed-related synchronous frequency affecting the shaft instability is distinctly observed in the frequency contour.

• Proceedings of the Korea Water Resources Association Conference
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• 2006.05a
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• pp.1561-1565
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• 2006

수제는 주로 호안 또는 하안 전면부에 설치하는 구조물로써 기존의 수제 설치는 하안 및 제방의 보호, 유로제어 및 주운 등의 목적에 의해 이루어졌다. 최근 들어서는 수제하류부의 흐름분리로 인해 발생되는 재순환 영역(recirculation zone)과 국부세굴에 의해 발생하는 세굴공이 수중생물의 다양한 서식처 및 홍수 시어류의 피난처로 활용될 수 있다는 점 등의 환경기능이 부각되면서 수제에 대한 설치목적이 다양화 되었다. 월류수제는 흐름이 수제 투과정도를 나타내는 투과율과 함께 다뤄지기는 기존의 실험연구에서는 수위가 수제의 머리부를 초과함에 따라 월류되는 흐름은 과도한 난류의 발생 등 투과수제에 비해 수제부근에 더 많은 영향을 미친다고 하였다. 이러한 과도한 난류의 발생은 수제를 월류하는 흐름은 상류에서는 가속되다가 수제 하류부로 흘러내리면서 다시 감속되어 교란되기 때문이다. 이러한 월류수제의 흐름특성은 수제 주변 국부세굴에 영향을 미친다. 특히 우리나라 하천은 홍수시 수위의 변화가 매우 크기 때문에 일반적인 불투과 수제라 하더라도 대부분의 수제가 월류수제처럼 거동한다. 따라서 수위가 증가함에 따라 월류가 발생하는 수제의 경우 비월류 구조물과는 세굴심의 변화가 다르게 발생할 수 있다. 본 연구에서는 월류수제 주변에서 발생되는 국부세굴이 수중생물의 다양한 서식처 및 피난처로 활용될 수 있다는 관점에서 세굴영역(세굴부피)과 세굴심의 관계에 대한 수리모형실험을 수행하고 분석하였다. 월류수제의 세굴실험은 축척의 영향을 최소화하기 위해 $7m(W){\times}40m(L){\times}1.5m(H)$ 규격의 대형 수로에서 수행하였으며 세굴변화에 미치는 시간축척의 영향을 파악하기 위해 $70{\sim}90$ 시간 동안 실험을 수행하였다. 세굴의 측정은 투명한 아크릴로 제작된 수제 내부에 CC카메라를 수제 전 후면 및 측면에 설치하여 월류수제의 세굴 발생을 실시간으로 측정하며 동시에 수제의 각 면에 각각 3개의 압력센서를 설치하여 압력분포를 측정함으로써, 월류수제 주변의 압력변화에 따른 세굴심의 실시간 변화를 비교할 수 있도록 하였다.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.35 no.7
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• pp.717-722
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• 2011

The aim of this study is to identify the locations at which local wall thinning occurs and to determine the turbulence coefficients related to local wall thinning. Experiments and numerical analyses of the tee sections of different down-scaled piping components were performed and the results were compared. Numerical analyses of full-scale models of actual plants were performed in order to simulate the flow behaviors inside the piping components. In order to determine the relationship between the turbulence coefficients and the rate of local wall thinning, numerical analyses of the tee components in the main feedwater systems were performed. The turbulence coefficients obtained from the numerical analyses were compared with the local wear rate obtained from the measurement data. From the comparison of the results, the vertical flow velocity component (Vr) flowing to the wall after separating in the wall due to the geometrical configuration and colliding with the wall directly at an angle of some degree was analogous to the configuration of local wall thinning.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.290-293
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• 2017

A direct-connected, continuous type combustion test facility was developed to test a supersonic combustor model used in scramjet engines. The facility requirements were determined by assuming the flight speed of Mach 5, yielding the combustor inlet flow speed of Mach 2. Also the cross-section of the supersonic combustor under test was assumed as $32mm{\times}70mm$. As a result, the facility was designed to have the flow total pressure of 548 kPaA, total temperature of 1,320 K, and flow rate of 0.776 kg/s. The facility consists of a turbo type air compressor, electric air heater, vitiation air heater and a two dimensional facility nozzle to accelerate the flow to Mach 2. Also, an oxygen supply system was added to compensate the vitiation. The exhaust de-pressurization system is not added. Designed pressure, temperature, and flow rate were verified through the test operation of the facility.

• Journal of the Korean Society of Propulsion Engineers
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• v.2 no.2
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• pp.64-73
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• 1998

In twin spool aero-engine, there may be a S shaped annular duct between high pressure and low pressure spools. The flow passing this S shaped duct experiences the flow acceleration and deceleration due to the convex and concave surface of the duct as well as the increase of blockage according to the boundary layer growth along the surfaces. So, the high pressure compressor which is located behind the S shaped duct is influenced by the non-uniform flow field generated by the geometry of inlet duct. To study the influence of the S shaped duct on the centrifugal stage, performance tests were implemented for the compressor with straight cylindrical inlet duct and with S shaped inlet duct, respectively. The test results showed that the performance, such as pressure ratio and efficiency, of the compressor with S shaped duct was worse than that of the compressor with cylindrical duct. And the compressor with S shaped duct had reduced maximum flow rate around design speed. To investigate the cause of performance degradation, flow anlaysis was performed for the impeller in front of which is located S shaped annular duct. The result of CFD showed the strong acceleration of the flow in the axial direction around the inducer tip region which caused the increase of relative mach number and the decrease of incidence angle of the flow.

• Journal of the Korean Vacuum Society
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• v.16 no.1
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• pp.46-51
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• 2007

The HFMX((High Flux Macromolecular X-ray crystallography) beamline at Pohang Accelerator Laboratory uses beams from a multi-pole wiggler. Two horizontal and vertical slits relevant to high heat-load are installed at its front-end. In order to treat high heat-load with reducing beam scattering, the horizontal slit has two Glidcop blocks with a grazing incidence angle of $10^{\circ}$ of a grazing-incidence knife-edge configuration. The blocks adjust the slit gap by being translated along guides by two actuating bars, respectively. Water flowing through holes, drilled along the actuating bars, cools the heat-load of both blocks. The vortical slit has the same structure as the horizontal slit except its installation direction with respect to the vacuum chamber and its grazing incidence angle. By virtue of a pair of blocks translating on guides, no alignment between both blocks is required and the installed slits show stable operating performance. The cooling performance of the two slits has been also shown to be acceptable. In this paper, the detailed explanation for the design of the two slits is presented and their operating performance is discussed.