• International Journal of Fluid Machinery and Systems
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• 제2권4호
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• pp.439-448
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• 2009

Three inducers were designed to avoid cavitation instabilities. This was accomplished by avoiding the interaction of tip cavity with the leading edge of the next blade. The first one was designed with extremely larger leading edge sweep, the second and third ones were designed with smaller incidence angle by reducing the inlet blade angle or increasing the design flow rate, respectively. The inducer with larger design flow rate has larger outlet blade angle to obtain sufficient pressure rise. The inducer with larger sweep could suppress the cavitation instabilities in higher flow rates more than 95% of design flow coefficient, owing to weaker tip leakage vortex cavity with stronger disturbance by backflow vortices. The inducer with larger outlet blade angle could avoid the cavitation instabilities at higher flow rates, owing to the extension of the tip cavity along the suction surface of the blade. The inducer with smaller inlet blade angle could avoid the cavitation instabilities at higher flow rates, owing to the occurrence of the cavity first in the blade passage and its extension upstream. The cavity shape and suction performance were reasonably simulated by three dimensional CFD computations under the steady cavitating condition, except for the backflow vortex cavity. The difference in the growth of cavity for each inducer is explained from the difference of the pressure distribution on the suction side of the blades.

• 한국산학기술학회논문지
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• 제21권5호
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• pp.623-629
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• 2020

본 연구는 항공기 기총발사 비행조건에서 Gun Port 주변 공기 유동장을 분석하여 디버터(Diverter) 옵션 형상에 따른 Gun Gas 유동량 및 경로를 확인하고 항공기 성능 및 안전성 영향을 확인하였다. Gun Port Diverter는 기총사격 시 발생하는 열을 효과적으로 낮춰주는 역할을 할 뿐아니라 Gun Gas를 상향방향으로 효율적으로 배출시키는 역할을 수행하며, 그 형상에 따라 Gun Gas 경로가 변경될 수 있다. 후방 Gun Port Diverter의 옵션 형상에 따라 기총 발사 시 Gun Gas의 유량, 경로, 압력을 분석하였다. Gun Port 내부 속도분포와 온도변화를 분석한 결과 후방 Diverter를 지나는 유량은 옵션 형상에 따라 급격이 감소하는 경향을 보이지만, 전방을 지나는 유량은 변화가 적은 비슷한 경향을 보임을 확인하였다. 따라서 기총발사 시 발생하는 Gun Gas는 후방 Gun Port Diverter 옵션 형상과 관계없이 항공기 표면에서 충분한 유동 거리가 확보되며, Diverter 옵션 형상에 따른 Gun Gas 유동의 정체는 Gun Port 내부 온도 상승에 큰 영향을 미침을 확인하였다.

• 한국터널지하공간학회 논문집
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• 제15권3호
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• pp.301-310
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• 2013

현재 도로터널에는 화재시 임계풍속을 유지할 수 있도록 제트팬을 설치하고 있으며, 제트팬 댓수는 임계풍속을 유지하기 위한 유동저항, 자연풍에 의한 환기저항, 열부력에 의한 환기저항을 고려하여 산정한다. 그러나, 국내의 경우, 제트팬 댓수 산정시 열부력은 고려하지 않고 있는 실정이다. 이에 본 연구에서는 열부력이 제트팬 댓수에 미치는 영향을 검토하기 위해서 터널연장(500, 750, 1000, 1500, 2000, 3500 m) 및 경사도(-1.0, -1.5, -2.0%)를 변수로 하여 화재성장곡선에 따른 비정상상태의 수치 시뮬레이션을 수행하였으며, 열기류의 평균온도 및 열부력에 의한 압력손실을 검토하여 열부력이 제트팬 댓수에 미치는 영향을 검토하였다. 이에 본 연구에서는 화재로 인한 열부력을 고려하는 경우에 제트팬 댓수의 증가가 필요하며, 특히, 설계화재강도를 100 MW로 하는 경우에는 본 해석조건의 모든 범위에서 열부력에 의한 압력손실이 차량저항에 의한 압력손실의 최대치보다 증가하며, 현행설계기준을 적용하는 경우보다. 최소 2~11대의 제트팬 대수의 증가가 필요한 것으로 분석되었다. 따라서 제연용 제트팬 용량 산정시 열부력에 대한 고려가 반드시 필요한 것으로 나타났다.

• 한국화재소방학회논문지
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• 제30권1호
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• pp.104-110
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• 2016

본 연구는 2012년도에 제정된 원심펌프 기준에 바탕을 둔 소방자동차용 소방펌프의 성능 인정 기준에 각종 초고층 건물의 화재 및 대형화재에 대비하기 위한 고압 및 대용량의 방수 능력을 가진 용적형 펌프의 인정기준 추가에 관한 내용이다. 용적형 펌프의 실험을 바탕으로 V-1, 2, 3급의 3가지에 대한 성능에 대하여 인정기준을 제정하였으며 펌프의 효율은 원심펌프형과 동일한 65% 이상의 성능을 요구하는 인정기준이 포함 되었다. 방수압력은 1.5 MPa~2.5MPa 사이의 값을 유량은 최소 $0.31m^3/min$에서 최대 $3.0m^3/min$의 방수량의 성능을 요구하는 것으로 제정되었다. 또한, 구조적으로 체절압력을 조절해야하는 용적형 펌프 특성상 릴리이프 밸브에 대한 부분이 추가되었으며 이물질로 인한 펌프 내부의 파손을 방지하기 위한 스트레이너 설치 및 진공펌프 없이 작동하는 용적형 펌프와 원심펌프와의 차이점을 포함하고 있다. 이와같은 용적형 펌프의 인정기준 부분 추가로 인하여 초고층 빌딩 및 대형화재에서의 화재진압에 있어서 보다 다양한 화재 진압용 소방 장비의 선택과 능동적인 대응을 할 수 있을 것으로 기대되며, 이와같은 인정기준은 2016년 1월 제정되었다.

• 한국유체기계학회 논문집
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• 제16권5호
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• pp.5-10
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• 2013

The regenerative pump is a kind of turbomachine which is capable of developing high pressure rise at relatively lower flow rates compared to the centrifugal and axial pumps. Although the efficiency of regenerative pumps is much lower than other turbomachines, still they have been widely used in many industrial applications for working at low specific speeds. There are some theoretical models to analysis the pump performance, however, the effect of the blade angle on the pump performance has not been covered in any model to date. In the present study, experimental study on the regenerative pump performance according to the impeller blade angle and its shape has been carried out. The straight radial blades with forward, backward and chevron blades which have inclined angles of $15^{\circ}$, $30^{\circ}$ and $45^{\circ}$ were tested. The pump performance characteristics as the pressure head, efficiency were obtained depending on the flow rate for every impeller, and their results, expressed in appropriate non-dimensional coefficients, were compared and analysed in detail. From the experimental results, it was found that the pressure head and the efficiency depend strongly on the blade angles as well as the blade type. These experimental data has made it possible to better understand the effects of the blade angle on the pump performance, and widen the applicability of the current performance analysis and design models with including the effect of blade angles.

• 한국가스학회지
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• 제16권5호
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• pp.7-13
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• 2012

알루미늄 분진폭발특성에 미치는 입경과 농도 변화에 따른 영향을 20 L 구형 분진폭발시험장치를 사용하여 실험적으로 조사하였다. 실험에 사용한 알루미늄 분진의 체적 평균 입경은 15.1 및 $34.8{\mu}m$이다. 실험결과, 평균 입경 $15.1{\mu}m$에서의 폭발하한농도(LEL)는 $40g/m^3$, 최대폭발압력($P_{max}$)은 9.8 bar, 폭발압력상승속도는 ($[dP/dt]_{max}$)는 1852 bar/s이었으며, 평균입경 $34.8{\mu}m$의 경우에는 LEL이 $70g/m^3$, $P_{max}$는 7.9 bar, $[dP/dt]_{max}$는 322 bar/s가 얻어졌다. Al분진의 폭발하한농도는 입경 증가에 따라 증가하는 경향이 관찰되었다. 또한 평균입경 $15.1{\mu}m$에서의 Al분진폭발압력으로부터의 화염전파속도의 계산값은 평균입경 $34.8{\mu}m$의 경우보다 5배의 크기를 나타내었다.

• The Korean Journal of Physiology
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• 제9권2호
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• pp.17-22
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• 1975

Adult nonpregnant female rabbits were subjected to the study of the effects of carbon monoxide inhalation on the uterine motility. Animals were anesthetized with intravenous injection of nembutal, 35 mg/kg, and the uteri were exposed. Polyethylene tubing which had a small hole near the blind tip was inserted in the loop and normal saline was infused at a constant rate of 1.5 ml/min. On the other end of the loop, an outlet of fluid was made. When a peristaltic wave proceeded to the hole, a rise of the pressure was ensued and it was transmitted to the pressure transducer, making an upward deflection of the recording pen on the physiograph. Carbon monoxide, 1,000 ppm in the concentration, was inhaled through a tracheal cannula for 30 minutes, following fresh air for 30 minutes. In some cases, pure oxygen was also supplemented for another 30 minutes. Uterine motility was expressed in terms of the impulse that was the time integral of the pressure and of the frequency of the peristaltic waves. The results obtained were as follows. 1. When 1,000 ppm carbon monoxide was inhaled for 30 minutes, the impulse dropped to $72{\pm}16.5%$ and the frequency to $75{\pm}22.7%$ of the values obtained before the gas administration. 2. By fresh air for 30 minutes, the impulse and the frequency restored to $77{\pm}25.7%$ and $92{\pm}21.1%$, respectively. 3. By the supplement of pure oxygen for 30 minutes, no remarkable improvement were revealed, showing $89{\pm}35.2%$ in the impulse and $91{\pm}10.8%$ in the frequency, respectively. 4. There was an appreciable discrepancy in the recovery courses of the impulse and the frequency, suggesting different mechanisms attributable to the alteration by carbon monoxide inhalation.

• 한국안전학회지
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• 제19권4호
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• pp.150-154
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• 2004

실린더형의 내용적 6리터의 용기를 이용하여 수소와 액화석유 가스(LPG)의 폭발 특성을 측정하였고 270리터의 직육면체 용기를 이용하여 폭발 후 화재로의 전이 현상을 실험하였다. 폭발 특성은 strain type 압력센서를 사용하여 측정하였으며 폭발 후 화재로의 전이 현상은 고속카메라로 촬영하여 분석하였다. 실험 결과 완전 연소 농도 비보다 약간 높은 농도에서 최대 폭발압력을 나타내었다. 폭발압력 상승 속도와 화염 전파속도는 연소속도와 비례함을 알 수 있었으며 이러한 폭발 특성들은 폭발 후 화재로의 전이에 영향을 미침을 알 수 있었다. 또한 폭발 화염온도, 화염의 용기 내 체류시간 등도 폭발 후 화재로의 전이에 중요한 변수가 됨을 알 수 있었다.

• 한국지구물리탐사학회:학술대회논문집
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• 한국지구물리탐사학회 2003년도 Proceedings of the international symposium on the fusion technology
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• pp.142-149
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• 2003

Blind hydraulic backfilling is a commonly used technique for subsidence control of the strata over unapproachable waterlogged underground excavations. In this investigation model studies on all the three variants of this technique, namely, hydro-pneumatic or air-assisted gravity backfilling, pumped-slurry backfilling and simple gravity backfilling, have been carried out in fully transparent models of the underground excavations. On examination of the filling process, it was revealed that in all the three cases, the basic process of filling occurs by sand transport along one or more meandering channels. The relative influence of sand, water and air flow rates on the area of filling from a single inlet point and the hydraulic pressure loss per unit length were studied in details. In hydro-pneumatic backfilling process, the air bubbles while moving upward through the meandering channels provide an additional buoyant force over and above the available hydraulic head. In this way the area of filling from a single borehole may be quite large even at small flow rates of water. During actual field implementation the injected air, if not released completely from the rise side holes, may cause troubles by way of creating potholes on the surface. The pumped-slurry technique has shown its capability of filling a relatively larger area at faster rate, especially when high-volume, low-pressure method was selected. But simple gravity filling was also found to be equally effective method as slurry pumping, especially when flow rates were high. In the second and third method discussed above, examination of variations of injection pressure was also done and its relation with physical phenomenon was also attempted. Some empirical relationships were also developed using multivariate regression with a view to help the practicing engineers.

• 한국수소및신에너지학회논문집
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• 제24권6호
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• pp.573-579
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• 2013

Hydrogen engine with homogeneous charged compression ignition can achieve high efficiency by high compression ratio and rapid chemical reaction rates spatially. However, it needs to expansion of the operation range with over-all load conditions which is very narrow due to extremely high pressure rise rate. The adoption of the lean boosting in a HCCI $H_2$ engine is expected to be effective in expansion of operation range since minimum compression ratio for spontaneous ignition is decreased by low temperature combustion and increased surround in-cylinder pressure. In order to grasp its possibility by using lean boosting in the HCCI $H_2$ engine, compression ratio required for spontaneous ignition, expansion degree of the operation range and over-all engine performance are experimentally analyzed with the boosting pressure and supply energy. As the results, it is found that minimum compression ratio for spontaneous ignition is down to the compression ratio(${\varepsilon}$=19) of conventional diesel engine due to decreased self-ignition temperature, and operation range is extended to 170% in term of the equivalence ratio and 12 times in term of the supply energy than that of naturally aspirated type. Though indicated thermal efficiency is decreased by reduced compression ratio, it is over at least 46%.