• 한국추진공학회지
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• 제5권3호
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• pp.19-24
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• 2001

대기중에서 움직이는 비행체(항공기, 미사일 등)의 속도 및 고도를 측정하기 위한 장치가 피토관 (Pilot-Tube)이다. 고속으로 비행하는 항공기의 안전하고 효율적인 운항을 위해서는 정확한 비행속도 및 고도측정이 요구된다. 피토관 최적 설계인자 결정을 위해 피토관 Nose의 Inlet부, Nose부 외곽형 상, 정압홀의 형상 및 정압홀 설치 위치 선정을 위한 유동장 해석을 수행하였다. 또한 해석을 통해 얻은 설계자료를 기본으로 제작한 피토관의 풍동실험을 수행하였다. 본 연구를 통해 속도 및 고도 계측용 피토관의 설계기술을 확보하였고 제작기술을 보유하였으며, 유동해석 및 풍동실험을 함으로써 피토관 국산화에 필요한 기본 자료를 얻었다.

• 한국자동차공학회논문집
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• 제12권2호
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• pp.91-100
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• 2004

Plate heat exchangers (PHE) have been widely used in different industrial applications, because of high heat transfer efficiency per unit volume. Basic study is performed for PHE to the application of intercooler in automobile. In order to understand the flow phenomena in the plate heat exchanger, a channel which was formed by the upper and lower plate in single plate was considered as calculation domains. Because chevrons attached on the upper plate are brazed with chevrons attached on the lower plate, the flow channel has very complex configuration. This complex geometry was analyzed by Fluent. In order to validate this methodology the proper experimental and theoretical data are collected and compared with numerical results. Finally, due to the lack of experimental values for PHE to the application of intercooler, various chevron angles and air velocities at inlet were tested in terms of physical phenomena. From this point of view, results of velocity vector, path lines, static pressure, heat flux, heat transfer coefficient, and Nusselt number are physically reasonable and accepted for the solutions. From these results, the correlations for pressure drop and Nusselt number with respect to chevron angle and Reynolds number in specific PHE are obtained for the design purpose. Thus, the methodology of the flow analysis in the full geometry of the channel was established for the predictions of performance in plate heat exchanger.

• 한국유체기계학회 논문집
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• 제19권2호
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• pp.5-10
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• 2016

Gas flow measurement in a closed duct was performed using multi-point Pitot tubes. Measurement uncertainty was assessed for this measurement method. The method was applied for the measurement of air flow into a gas turbine engine in an altitude engine test facility. 46 Pitot tubes, 15 total temperature Kiel probes and 9 static pressure tabs were installed in the engine inlet duct of inner diameter of 264 mm. Five tests were done in an airflow range of 2~10 kg/s. The flow was compressible and the Reynolds numbers were between 450,000 and 2,220,000. The measurement uncertainty was the highest as 6.1% for the lowest flow rate, and lowest as 0.8% for the highest flow rate. This is because the difference between the total and static pressures, which is also related to the flow velocity, becomes almost zero for low flow rate cases. It was found that this measurement method can be used only when the flow velocity is relatively high, e.g., 50 m/s. Static pressure was the most influencing parameter on the flow rate measurement uncertainty. Temperature measurement uncertainty was not very important. Measurement of boundary layer was found to be important for this type of flow rate measurement method. But measurement of flow non-uniformity was not very important provided that the non-uniformity has random behavior in the duct.

• 방사성폐기물학회지
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• 제2권3호
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• pp.201-209
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• 2004

파일럿 규모의 유리화플랜트에서 일련의 시험을 통해 고온 세라믹 캔들 필터 시스템의 주요 운전 변수 및 성능을 평가하였다. 실증 시험결과 매 시험초기에는 필터 표면 먼지층(Dust cake)의 생성으로 인해 필터 매질에 걸리는 차압이 급격히 상승하였다. 그런 다음 차압은 곧 일정한 범위에서 안정되었고, 표면유속(Face velocity)에 비례하여 계속적으로 변화하였다. 이와 반대로, 필터 투과율(Permeability)은 매시험 초기에 급격히 감소하였다. 필터표면 먼지의 역세정은 공기압 3～5 bar범위 일때 효율적이었다. 필터 입구 및 출구에서 동시에 등속으로 채취한 먼지농도를 바탕으로 필터의 먼지 포집율(Dust collection efficiency)을 평가한 결과 필터 성능은 설계값인 99.9%과 같은 것으로 나타났다. 100시간의 장기시험을 포함한 일련의 실증시험을 수행하는 동안 고온 필터 시스템의 성능에 영향을 주는 특별한 문제점은 발견되지 않았다.

• 한국자동차공학회논문집
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• 제19권6호
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• pp.61-67
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• 2011

The cooling module needs enough space (or distance) from hood to absorb the energy from any pedestrian collision. Downsized cooling module for pedestrian protection is important to reduce the severity of pedestrian injury. When a vehicle collision happens, the downsized cooling module is required to reduce the risk of injury to the upper legs of adults and the heads of children. In this study, the performance of cooling module to cool the engine was investigated under 25% height reduction. The heat dissipation and pressure drop characteristics have been experimentally studied with the variation of coolant flow rate, air inlet velocity and A/C operation ON/OFF for the downsized cooling module. The results indicated that the cooling performance was about 94% level compared to that of the conventional cooling module. Therefore, we checked that the cooling module had good performance, and expected that the cooling module could meet the same cooling performance as conventional cooling module through optimization of components efficiency.