• Journal of KSNVE
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• v.11 no.1
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• pp.15-20
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• 2001

홴(fan)은 모터로부터 회전력을 전달받아 공기동력인 풍량과 정압을 발생시켜 발열부품의 냉각 및 환기용으로 산업현장과 가전기기에서 널리 사용되고 있다. 과거 산업현장에서 주로 사용되어지던 송풍기가 가전기기에 적용되면서 홴에 대한 관심이 더욱 증폭되었는데 특히 국내에서 독자적인 소형 홴 연구가 본격적으로 시작된 것도 이 때이다. 가전에서의 홴은 고효율 뿐 만 아니라 주로 저소음화에 대한 연구에 초점이 맞추어져 있는데 이는 기존의 산업현장의 송풍기가 주로 풍량과 정압에 목표를 두고 개발해 왔던 것도 한 이유지만 구조적인 안정성 때문에 소음을 고려한 설계가 한계가 있었기 때문으로 저소음홴에 대한 응용기술이 충분히 발달하지 못했기 때문에 송풍기 기술을 그대로 받아들인 초창기 가전용홴은 소음이 높았다. 또한 가전기기는 모든 연령층이 사용하기 때문에 소음이 큰 제품은 항상 소비자 클레임의 원인이 되기 때문이다.(중략)

• Aerospace Engineering and Technology
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• v.2 no.2
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• pp.25-32
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• 2003

In the present paper, a computational study on the hydrodynamic behavior of the inducer are presented including the effect of the mass flow rate. The adopted inducer showed very low head rise with high volume flow rates, which may be caused by the small passage area near the trailing edge. The static pressure distributions at the shroud surface are compared with experimental results showing very good agreements. The overall performance of the inducer such as, efficiency, head rise is also compared with experiments. The computational results are generally in good agreements with experimental ones near the design point, but at the high flow rate, the two results shows discrepancy.

• Proceedings of the KSME Conference
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• 2001.06d
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• pp.715-720
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• 2001

The main reason for applying positive pressure variable clearance packing in fossil power plant is high efficiency and energy saving movement in the government. This study intends to analyze the turbine efficiency through the shaft packing improvement in thermal power plant and makes its comparison to that of the used packing.

• Proceedings of the Korean Vacuum Society Conference
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• 2013.08a
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• pp.300.1-300.1
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• 2013

반사방지막 코팅(Anti-reflection coating)은 태양전지(Solar cell), 발광다이오드(LED) 등의 반사율을 낮추어 효율을 증대시키기 위하여 사용되고 있다. 본 실험에서는 유리 기판 위에 실리콘 타겟을 이용한 Reactive magnetron sputtering 장비를 활용하여, 50~100 mTorr의 높은 공정 압력(High pressure)에서 증착하여 SiO2 반사방지막 코팅층을 형성하였다. Ellipsometer를 이용하여 SiO2 박막층의 굴절률(Refractive index)을 측정한 결과, 공정 압력에 따라 SiO2 박막이 다양한 굴절률을 가지는 것을 확인할 수 있었다. 또한, UV-Vis spectrometer를 이용하여, 450~600 nm 파장에서의 반사율(Reflectance)과 투과율(Transmittance)을 측정하여 비교, 분석하였다. 나아가 증착된 SiO2 반사방지막을 비정질 실리콘 박막 태양전지에 적용하여 효율 향상 효과를 실험하였다. 이를 활용하여 낮은 굴절률을 갖는 반사방지용 SiO2 코팅층을 형성하여 태양전지의 광 변환 효율을 상승 시킬 수 있고, 발광다이오드의 광 추출 효율을 증가시킬 있을 것으로 여겨진다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.05a
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• pp.295-298
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• 2009

Bent ducts add loss and decrease efficiency. Many researchers have been conducted the performances of bent ducts, but their shapes of inlet and outlet are same. However, in this investigation, the focus is on a bent duct which is annular at the inlet and circular at the outlet. The bent duct of these complex shapes has not been investigated, but has been used in many fields. The performance of such bent duct is investigated under inlet speed 54 m/s and Re = 238,000. Wall static pressure tappings are located surface of the bent duct to measure the static pressure and a probe is traversed at the inlet and outlet of the bent duct to measure the total pressure. As a result, it presents static pressure distribution on the bent duct surface, streamwise velocity profile at inlet and outlet of the bent duct and total pressure loss profile at outlet. In this investigation, the total pressure loss coefficient is 0.243.

• Journal of the Korean Society of Propulsion Engineers
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• v.5 no.3
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• pp.19-24
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• 2001

The Pilot-Tube is the device that measures velocity and altitude of high speed vehicle. Accurate measurements of speed and altitude are essential to the safe and efficient operation of aircraft. For the purpose of determining optimal design parameters of Pilot-Tube such as nose inlet configuration, nose shape, static hole configuration, and static hole location, subsonic flow field was calculated numerically and analyzed. A Pilot-Tube was manufactured based on numerical flow field analysis, and pressure and air velocity was measured experimentally in the wind tunnel. As a result manufacturing and design technologies of the Pilot-Tube were acquired to make flight-device.

• Journal of the Korean Society of Mechanical Technology
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• v.13 no.1
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• pp.31-40
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• 2011

This study was conducted to research how UCD(Ultra Constant Discharge) lamp lighting affects plant cultivation. To get the results within a short time, lettuce seedling was selected as a plant and nutrient hydroponic beds were used in a dark room for 100% artificial lighting. Two beds were installed for same distance lighting condition with UCD lamp and Hi-pressure Sodium lamp each and another two beds were installed for same light intensity condition with each type of lamp. After 15 days of cultivation, for both conditions, the yields under UCD lamp were weighed more than that under Hi-pressure Sodium lamp. The result can be analyzed that the spectrum of UCD lamp having near sunlight characteristic is much superior to that of Hi-pressure Sodium lamp having a line spectrum characteristic on yellow and red wavelengths for plant cultivation.

• Proceedings of the KSME Conference
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• 2004.11a
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• pp.1676-1681
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• 2004

The main reason for applying positive pressure variable clearance packing in fossil power plant is high efficiency and energy saving movement in the government. This study intends to analyze the turbine efficiency through the shaft packing improvement in thermal power plant and makes its comparison to that of the each packing type

• Proceedings of the Korea Committee for Ocean Resources and Engineering Conference
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• 2001.05a
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• pp.240-243
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• 2001

괘도차량에 부착된 물분사추진기의 유동해석을 실험과 포텐셜해석 그리고 점성해석을 사용하여 그 결과를 비교하였다. 예인수조에서 여러 차량 전진속도에 대해서 임펠러 회전수를 조정하여 제트속도를 변화시키면서 덕트표면에서의 정압을 계측하였다. 이는 제트시스템의 효율을 추정하기 위함이고 관로를 통한 에너지분포를 알 수 있다. 점성유동해석을 위해 지배방정식은 비압축성 Navier-Stokes 방정식을 유한체적법을 사용하여 이산화하고 해석하였으며 난류영향은 표준 ĸ-$\varepsilon$난류모형을 사용하여 유동을 해석하고 실험결과 및 포텐셜 해석결과와 비교하였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.31 no.6
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• pp.72-78
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• 2003

In the present paper, computational studies on the hydrodynamic behavior of the inducer for the rocket-engine turbopump are presented including the effect of the mass flow rate. As the mass flow rate is increased, the inducer showed better performance with weak back flows which may have deleterious effects upon the anti-cavitation ability. But the adopted inducer showed low head rise with high volume flow rates, which may be caused by the small passage area near the trailing edge. The static pressure distributions at the shroud surface are compared with experimental results showing very good agreements except near the leading edge where strong back flows are present. The overall performance of the inducer such as, efficiency, head rise is also compared with experiments. The computational results are generally in good agreements with experimental ones near the design point, but two results show discrepancy at the high flow rate.