• International Journal of Fluid Machinery and Systems
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• 제10권2호
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• pp.176-188
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• 2017

The nozzle-flapper valves are widely applied as a pilot stage in aerospace and military system. A subject of the analysis presented in this work is to find out a reasonable range of null clearance between the nozzle and flapper. This paper has presented a numerical flow coefficient simulation. In every design point, a parameterized model is created for flow coefficient simulation and cavitation under different conditions with varying gap width and inlet pressure. Moreover, a new test device has been designed to measure the flow coefficient and for visualized cavitation. The numerical simulation and test results both indicate that cavitation intensity gets fierce initially and shrinks finally as the gap width varies from small to large. From the curve, the flow coefficient mostly has experienced three stages: linear throttle section, transition section and saturation section. The appropriate deflection of flapper is recommended to make the gap width drop into the linear throttle section. The flapper-nozzle null clearance is optionally recommended near the range of $D_N/16$. Finally through simulation it is also concluded that the inlet pressure plays a little role in the influence on the flow coefficient.

• 대한기계학회논문집B
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• 제23권2호
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• pp.166-174
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• 1999

The flow characteristics of 2-valve and 4-valve cylinder heads with various blocked-valve were experimentally investigated in a steady flow rig. Effects of the blocked-valve configurations on flow coefficient, swirl and tumble intensity are studied. Compared to the conventional valve, the blocked valve in both cylinder heads have the much lower flow coefficient and the much higher intensity of swirl and tumble. Under the same size of blockage, the value of flow coefficient and swirl(or tumble) intensity were varied according to the position of blockage. Throughout these steady flow test the optimized positions of blockage in both cylinder heads were determined.

• 한국방재학회 논문집
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• 제11권1호
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• pp.67-75
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• 2011

본 연구에서는 우리나라의 남해안 및 서해안으로 유입되는 주요 하천인 낙동강, 섬진강, 금강을 대상으로 다목적 댐 건설과 같은 하천환경의 변화가 하천의 상 중 하류부에 미치는 영향에 대하여 검토하기 위하여 비교적 수위자료와 수위-유량곡선 자료가 잘 구비되어 있으며, 자료의 보유년수, 관측개시일 등 양질의 자료가 축적되어 있는 지점을 대상으로 다목적 댐의 건설 시점을 기준으로 유황분석을 실시하였다. 유황의 변화를 분석한 결과 낙동강 중류부에 위치한 적포교 지점을 제외한 모든 지점에서 풍수량, 평수량, 저수량, 갈수량이 증가한 것으로 나타났으며, 하류부의 유황개선효과가 중 상류부에 비해 큰 것으로 나타났다. 하상계수와 유황계수 또한 감소된 것으로 나타났으나 유황계수의 감소폭은 하상계수에 비해 작게 나타났다. 이는 유황계수가 유량의 극치값에 대한 영향을 하상계수에 비해 작게 받기 때문인 것으로 사료되며, 본 연구를 통해서 중 상류부에 위치한 다목적 댐의 긍정적인 효과를 확인할 수 있을 것이라 판단된다.

• 한국추진공학회지
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• 제21권4호
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• pp.89-95
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• 2017

본 논문에서 극저온 추진제를 사용하는 액체추진기관의 재순환예냉 시스템 설계의 유연성을 확보하기 위한 연소기 산화제 개폐밸브 재순환예냉 유로의 유량계수 개선 내용을 소개하였다. 밸브의 재순환 예냉 출구 포트 크기와 밸브 내부 유로 형상 변경에 의한 재순환예냉 유로의 유량계수 값을 예측하기 위해서 기존 밸브에서 측정한 재순환예냉 유로의 유량계수 값들을 활용하였으며, 액체질소를 운용유체로 사용하여 측정한 유량계수와 예측값과의 비교를 통해 밸브 내부 형상 변경에 의한 유량계수 개선정도를 확인하였다. 연소기 산화제 개폐밸브의 재순환예냉 유로의 유량계수는 기존 밸브에 비해 2배가량 향상되었으며, 결과적으로 연소기 산화제 개폐밸브에 할당되었던 설계 요구 차압의 75%가량을 재순환예냉 시스템에서 추가적으로 소요될 수 있는 잠재적인 차압과 재순환예냉 시스템의 다른 구성품의 추가 차압으로 활용될 수 있을 것으로 기대된다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 춘계학술대회논문집D
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• pp.528-533
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• 2001

An experimental study is carried out to investigate the effects of air and water mass flow rates on cooling characteristics of mist impinging jet on a flat plate. Experiments are conducted with air mass flow rates from 0.0 to 3.0 g/s, and water mass flow rates from 5.0 to 20.0 g/s. An air-atomizing nozzle is used for the purpose of controlling air and water mass flow rates. In this study, a new test section is designed to obtain local heat transfer coefficient distributions. Heat transfer characteristics of the mist impinging jet are explained with the aid of flow visualization. Surface temperature and heat transfer coefficient distributions become more uniform as air mass flow rate increases, and that the increases in water flow rate mainly enhance cooling performance. Air mass flow rate weakly influences averaged heat transfer coefficient when water mass flow rate is low, but averaged heat transfer coefficient increases remarkably as air mass flow rate in case of high water mass flow rate.

• 한국안전학회지
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• 제25권6호
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• pp.22-27
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• 2010

Flow Coefficients of intake port in an engine cylinder head were measured by a newly designed flow rig. In measuring the flow coefficient with traditional method, the valve lift was manually varied by technician with adjusting a micrometer which is directly connected to the intake valve of the cylinder head. The cam shaft of the cylinder head is directly rotated by a step motor and the valve lift was automatically varied with cam shaft profile in the newly designed flow rig. The measurement of the flow coefficient was automated by rotating the cam shaft with the step motor. Automatic measurement of the flow coefficient could be safely measured by separating a technician from the noise and vibration of the traditional flow rig. Also, the automatic measurement of the flow coefficient reduce the measurement time and provide meaningful statistical data.

• 한국기계가공학회지
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• 제15권2호
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• pp.16-21
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• 2016

This study is a numerical analysis of the flow characteristic of a quick coupler. The quick coupler is a popular coupling tool for pipelines in hydraulic and pneumatic systems. In this study, the flow characteristic of a quick coupler outlet is conducted about the flow coefficient. The quick coupler is analyzed for improving flow and confirmed with the study results. The velocities with pressure distribution according to inlet and outlet pressure drop of the coupler are also compared. The flow coefficient is analyzed according to the flow analysis result for each pressure drop. When the pressure drop is 1 psi, the flow coefficient (Cv) matched about 98% of the value provided by the actual product.

• 한국자동차공학회논문집
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• 제7권8호
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• pp.76-82
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• 1999

The object of this study is to find new evalution index for in-cylinder flow characteristics insteady of current swirl, tumble coefficient using steady flow test rig on intake port system. To this end, port flow rig test was conducted on DOHC head varying intake valve lift respectively. Finally combination angular coefficient and inclination angle were introduced as new evaluation index for in-cylinder angular flow characteristics.

• International Journal of Aeronautical and Space Sciences
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• 제3권1호
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• pp.1-8
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• 2002

A numerical analysis was performed on the fluid flow in injector orifice of a liquid rocket engine. The present computational code was verified against the published data for turbulent flow in a pipe with a sudden expansion-contraction. Considered were the parameters for the flow analysis in an injector orifice: Reynolds number, ratio of mass flow rate of the injector orifice and inlet flow rate, and slant angle of the injector orifice. The discharge coefficient increased slightly as the Reynolds number increased. The slant angle of the injector changed critically the discharge coefficient. The discharge coefficient increased by 7% when the slant angle changed from $-30^{\circ}$ to $30^{\circ}$ The ratio of mass flow rate had relatively little impact on the discharge coefficient.

• 한국자동차공학회논문집
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• 제6권6호
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• pp.113-131
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• 1998

The objective of the present study is to investigate the characteristics of the dividing flow in the laminar flow region. Using glycerine water solution(wt43%) for Newtonian fluid and the polymer of viscoelastic fluid(500wppm) for non-Newtonian fluid, this research investigates the flow state of the dividing tube in steady laminar flow region of the two dimensional dividing tube by measuring the effect of Reynolds number, dividing angle, and the flow rate ratio on the loss coefficient. In T- and Y-type tubes, the loss coefficients of the Newtonian fluid decreases in constant rate when the Reynolds number is below 100. The effect of the flow rate ratio on the loss coefficients is negligible. But when the Reynolds number is over 100, the loss coefficient with various flow rate ratios approach an asymptotic value. The loss coefficient of the non-Newtonian fluid for different the Reynolds number shows the similar tendency of the Newtonian fluid. And when the Reynolds number is over 300, the loss coefficient is approximately 1.03 regardless of flow rate ratio or the dividing angle. The aspect ratio does hardly influence the reattachment length and the loss coefficient of both Newtonian and non Newtonian fluid. The loss coefficient decreases as the Reynolds number increases. The loss coefficient of Newtonian fluid is larger than that of non-Newtonian fluid.