• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2008.05a
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• pp.263-267
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• 2008

In this work the realistic install performance analysis of a helicopter was performed together with power extraction enabling to operate auxiliary system as well as intake pressure loss, loss due to bleed air, etc. which must be considered in practical propulsion system's performance modelling to be installed to the airframe. The pressure loss occurring in intake was estimated from the intake performance map with relationships of Mach Number and pressure loss. In order to evaluate the proposed installed performance model, the experimental data for comparison must be needed when mounted in propulsion system. However because of lack of accessibility to such real data at the moment, the alternative way was made through comparison that the analysis results by the proposed model were compared with a wellknown commercial program GASTURB's analysis results. The validity of the proposed installed performance model was consequently confirmed because its average deferences from the GASTURB's results were within 0.5%.

• Journal of the Korean Society of Propulsion Engineers
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• v.12 no.1
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• pp.51-56
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• 2008

In this work the realistic install performance analysis of a helicopter was performed together with power extraction enabling to operate auxiliary system as well as intake pressure loss, loss due to bleed air, etc. which must be considered in practical propulsion system's performance modelling to be installed to the airframe. The pressure loss occurring in intake was estimated from the intake performance map with relationships of Mach Number and pressure loss. In order to evaluate the proposed installed performance model, the experimental data for comparison must be needed when mounted in propulsion system. However because of lack of accessibility to such real data at the moment, the alternative way was made through comparison that the analysis results by the proposed model were compared with a wellknown commercial program GASTURB's analysis results. The validity of the proposed installed performance model was consequently confirmed because its average deferences from the GASTURB's results were within 0.5%.

• Proceedings of the Korea Water Resources Association Conference
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• 2008.05a
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• pp.1828-1832
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• 2008

우수 관거 시스템에서 흐름은 중력에 의해서 흐르고 개수로 흐름과 같이 처리된다. 그러나 유입유량이 관거의 만관 상태를 초과하거나 하류 흐름의 제한 때문에 발생하는 역류의 영향을 받는다면, 우수 관거 시스템은 과부하(surcharge) 상태의 압력흐름이 된다. 개수로 상태에서 맨홀에서의 수두 손실은 일반적으로 무시되지만, 과부하 맨홀에서의 수두손실은 중요하며, 우수 관거 시스템의 전체 손실에 중요한 부분을 차지하게 된다. 이러한 현상은 여러 개의 맨홀을 가지는 우수 관거 시스템에서 특히 중요한 사항이 된다. 현재 계획 또는 설계단계에서 수행되고 있는 관거 시설의 수리계산에서는 연결관의 마찰손실만을 감안하여 수행하고 있으며, 맨홀에서의 수두손실은 고려되지 않는 실정이다. 본 연구에서는 일반적으로 3차원 유체거동의 특성분석에 많이 사용되는 Fluent 모형을 이용하여 과부하 원형 맨홀에서의 흐름특성을 수치모의 하였으며, 맨홀내 손실수두의 변화를 계산하여 손실계수를 산정하였다. 계산된 손실계수는 수리모형 실험을 통하여 산정된 손실계수와 비교하였다. 수치 모형에 의해서 산정된 손실계수 값이 수리모형 실험에 의해서 산정된 손실계수 값보다 약간 크게 산정되었다. 앞으로 난류 모형의 매개 변수들의 조정을 통한 정확한 수치모의 연구가 필요하다고 판단된다.

• Journal of the Korean Society of Propulsion Engineers
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• v.13 no.5
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• pp.29-40
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• 2009

Pneumatic system is widely applied to ground facility and launcher on-board system. One of the important aspects of pneumatic system is to meet pressure and flow rate requirements of gas consumers. In this paper, a systematic analytical approach for pneumatic system is proposed, which uses and systematically combines previous studies. The proposed analytical method is that pressure/flow calculation using conservation equations are combined with sonic limit check at vena contracta of the components of pneumatic system, which checks the installed components whether they are merely pressure loss elements or flow limiting element of the system. In this paper, gas consumers are categorized and simulated using the proposed method. The results reveal that the feeding performance of general pneumatic system can be properly estimated using the proposed approach.

• Journal of the Korean Society of Propulsion Engineers
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• v.18 no.5
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• pp.19-28
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• 2014

Firing test of solid rocket motor with pintle-technology carried out and the measured pressure-time curve was compared with the values predicted by the internal ballistic and performance analysis. Without baffle, the measured combustion chamber pressure was similar with the predicted pressure at the beginning of combustion, but gradual increase in pressure, which was unexpected with the end-burning grain of which burning area is constant, was observed. A baffle was inserted to make uniform flow over the pintle. Unlike the thruster without baffle, the measured combustion chamber pressure was 1.4 times higher than the predicted value. Through the CFD simulation, 10% of total pressure loss of the flow was observed from combustion chamber to nozzle throat when the baffle was inserted. The measured pressure with baffle was predicted well by considering the total pressure loss in the internal ballistic modelling and performance analysis.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.19 no.6
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• pp.27-36
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• 2018

A significant amount of studies were performed on evaporation heat transfer and pressure drop in microfin tubes. Most studies, however, focused on the refrigerants used in air-conditioners or heat pumps, and very limited information is available on R-404A, which is used in low temperature refrigeration. In this study, the evaporation heat transfer and pressure drop characteristics of R-404A in a 9.5 mm O.D. microfin tube were investigated for the mass flux range from $80kg/m^2s$ and $200kg/m^2s$. A smooth tube of the same outer dimeter was also tested for comparison. The results showed that the heat transfer enhancement ratio of the microfin tube increased with increasing mass flux and the heat flux decreased. The relative contribution of the convective heat transfer and the heat flux on total heat transfer was attributed to the observed trend. The pressure drops of the microfin tube were slightly (maximum 28%) larger than those of the smooth tube. Existing correlations do not adequately predict the measured heat transfer coefficients of pressure drops, probably due to the test range of the present study, which is outside of the existing correlations.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.33 no.2
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• pp.521-528
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• 2013

Urban drainage systems are generally designed as open channel flow. The system, however, shows a partially surcharged flow in its body, especially at junctions or manholes. Thus, a special case of this condition needs to be explained as pressurized flow condition for designing the sewer system. This study considered the surcharged manhole flows during an unexpected rainfall event or an excess of design frequency. Overflows from surcharged manholes and urban flooding can occur from the effect of surcharged flows. Thus, sewer systems should be designed with the concept of open channel flow and pressurized flow. Also, energy losses in a manhole need to be considered. The aim of this study is to develop the numerical model which can evaluate the effect of the energy losses at the manhole. The numerical model was verified and compared with hydraulic model and SWMM. The results showed that the water depth of numerical model was in good agreement with hydraulic model at the each manhole. However, the SWMM underestimated the water depth because that model ignored the energy losses at manholes. Thus, the developed numerical model in this study could be a useful tool for the assessment of a conveyance of urban drainage system.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2008.11a
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• pp.158-163
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• 2008

Muffler design in the exhaust system is critical to provide for low noise in shipboard spaces. In an attempt to effectively design the low noise muffler, it is important to evaluate the performance of the muffler considering not only the noise, but also pressure drop as well. For this purpose, a test system of large exhaust muffler for ship propulsion systems was designed based on ISO 7235. The substitution test for determining both the insertion loss and pressure drop of mufflers was carried out. A ship exhaust muffler is considered as a test example and the insertion loss and pressure drop are obtained.

• Proceedings of the Korean Nuclear Society Conference
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• 1997.05a
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• pp.279-285
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• 1997

본 연구에서는 나선형과 판형의 핀을 가진 원자력 발전소용 직교류 핀-관 열교환기의 열량을 ARI Standard-410에 따라 실험적으로 측정하여 풍속과 냉수속에 따른 열저항 및 압력 손실을 도출하는 것을 목적으로 하였으며, 이러한 시도를 통해서 실제 열교환기의 성능 평가시 필요한 기술적 자료를 축적하고자 하였다. 실험에서는 나선형 6fin/in, 8fin/1n, 10fin/in 열교환기와 판형 8fin/in 열교환기를 사용하였으며, 풍속을 0.486m/s와 2.214m/s로, 수속을 1m/s～4m/s로 하여 실험을 행하였다. 실험 결과를 통하여, 원자력 발전소의 격납 용기내의 공기조화를 위하여 사용되어 지는 열교환기의 성능 평가 방법 및 실증 능력을 확보하였으며, 풍속 증가에 따라 총괄 열전달 계수는 전체적으로 비례 증가하는 경향을 보였다. 판형이 나선형 보다 열전달 계수가 작게 나타났으며, 나선형 열교환기의 경우 fin수에 따른 변화는 크지 않았으나, 열전달 면적을 고려한 경우에는 나선형 10fin/in 열교환기가 가장 뛰어난 열교환 성능을 발휘함을 알 수 있었다. 또한, 공기측의 압력 손실은 전체적으로 전연 풍속 증가에 따라서 속도 제곱에 비례하여 증가하는 경향을 보였다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.05a
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• pp.341-344
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• 2009

본 연구에서는 허브 대 팁의 비가 큰 원심형 압축기의 성능시험을 수행하였으며, 이를 수치해석 결과와 비교하였다. 압력비의 경우 작동 회전수에서 성능시험과 수치해석의 결과의 경향이 일치하는 것을 확인하였다. 성능시험에서 임펠러의 성능은 매우 높게 나타났으나, 1단 및 2단 디퓨져에서 손실이 발생하여 전체적인 압력비 및 효율이 떨어지는 것을 확인하였다. 수치해석을 통해 내부 유동장을 확인한 결과 1단 디퓨져 및 2단 디스월러에서 격렬한 2차 유동으로 인한 유로차폐효과가 주 손실원인임을 확인하였다.