• 제목/요약/키워드: Jet A-1

검색결과 1,494건 처리시간 0.026초

Plasma Jet의 동축평행 자계에 의한 영향에 관한 연구 ( 1 ) (A Study on the Influence of Coaxial Parallel Magnetic Field upon Plasma Jet)

  • 전춘생
    • 전기의세계
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    • 제22권2호
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    • pp.57-69
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    • 1973
  • The aim of this study was to investigate the behaviors of plasma jet under coaxial magnetic field in paralled with it for controlling optical characteristics and input power of plasma jet without impurity and instability of arc plasma column. Because the discharge characteristics of plasma jet were so distinctively different according to the existence or non-existence of magnetic field, the input power, luminous intensity of plasma jet and thermal efficiency were comparatively studied in respect of such variables as arc current, gap of electrode, quantity of argon flow, magnetic flux density, diameter and length of nozzle, with the use of several materials which were different in diameter and length of nozzel. The results were as follows; 1) The voltage tends to show a drooping characteristic at law current and then rises gradually. The luminous intensity of plasma jet increases exponentially with arc current. 2) Arc voltage increases and luminous intensity tends to decrease gradually as gap of electrode increases. 3) Arc voltage and luminous intensity tends to decrease gradually as gap of electrode increases. 3) Arc voltage and luminous intensity increase in accordance with the quantity of argon flow. 4) At first step, arc voltage increases to maximum value with the growth of flux density and then tends to show a gradual decrease. Luminous intensity decreases with the growth flux density. 5) Arc voltage decreases as the constriction length of nozzle increases, maximum decrease is shown at the constriction length of 20(mm) and it increases beyond that value. The luminous intensity decreases as the constriction length grows. 6) Arc voltage and luminous in tensity increase with the growth of diameters of nozzle. 7) Thermal efficiency has values between 50% and 75%, being influenced by arc current, the quantity of argon flow, flux density, the length of electrode gap and the constriction length of nozzle.

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고온 세라믹필터의 펄스젯 탈진 성능에 관한 연구 (A Study on the Performance of Pulse Jet Cleaning in High Temperature Filter)

  • 김병렬;박승철;박병철;조현준;오형모;황태원;신상운
    • 방사성폐기물학회지
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    • 제3권1호
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    • pp.9-16
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    • 2005
  • To evaluate parameters influencing on the dust removal of the High Temperature Filter(HTF) system, a computer simulation of fluid dynamics inside the system had been performed. The results showed that the optimum pulse jet periods were 50ms and 90ms for the 1000mm and 1500mm long filter elements respectively. Dust removal effect was very excellent under the pulse jet pressure of 3 bar. But the distance between the pulse jet nozzle and the venturi of a filter element had no meaningful effect on the performance with the variation from 5mm to 10mm. Compared to the dispersion mode of pulse jet, the collective mode of pulse jet flow was preferable in maintaining the pressure inside the system stable.

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이중분사 홀의 면적비와 분사각 변화에 따른 가스터빈 막냉각 특성 연구 (A Study on the Film-cooling Characteristics of Gas Turbine Blade with Various Area Ratios and Ejection Angles of the Double Jet Holes)

  • 조문영;이종철;김윤제
    • 한국유체기계학회 논문집
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    • 제17권3호
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    • pp.59-64
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    • 2014
  • The kidney vortex is the important factor adversely influencing film cooling effectiveness. In general, double jet film-cooling hole is designed to overcome the kidney vortex by generating anti-kidney vortices. In this study, the film cooling characteristics and the effectiveness of the double jet film cooling hole were numerically investigated with various area ratios of the first($A_1$) and second($A_2$) cooling hole($A_1/A_2$=0.8, 1.0, 1.25) and lateral ejection angle(${\alpha}$ = $30^{\circ}$, $45^{\circ}$, $60^{\circ}$) as the design parameters. The effects of lateral distance between the first and second row holes are investigated. Numerical study was performed by using ANSYS CFX with the shear stress transport(SST) turbulence model. The film cooling effectiveness and temperature distribution were graphically depicted with various flow and geometrical conditions.

반복된 제트 충돌을 갖는 내부 유로의 평균 열전달 계수 측정 (Heat transfer coefficient measurement in the Blockage channel with Repeated Jet Impingement)

  • 박승덕;이기선;김석범;조용화;전창수;곽재수;허재성
    • 항공우주시스템공학회지
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    • 제2권4호
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    • pp.7-12
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    • 2008
  • Averaged heat transfer coefficients were measured in a turbine blade internal cooling passage model with three blockage walls. Each blockage wall was equipped with 9 staggered holes or slots in order to create different shaper of repeated jet impingement. The effect of jet shape on the averaged heat transfer coefficient was studied by the copper-thermocouple method and three Reynolds number of 10,000, 20,000, and 30,000 were tested. Results showed that the repeated stagger jets could increase the averaged heat transfer coefficient by at least 9 times compared to the smooth channel cases. Due to the large pressure drop induced by the repeated jet impingement, the thermal performance was less than 1 for all cases and decreased as the Reynolds number increased. Among the tested cases, the widest slot showed the best thermal performance. The measurement results showed that the thermal performance of the heat transfer augmentation by repeated stagger jets could be improved by altering the jet shape, and other shape of impingement jet will be studied in near future.

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PSP를 이용한 Cavity 후류의 전역적 압력분포 측정 (The Whole Region Pressure Measurement of Cavity Downstream using PSP Technique)

  • 김기수;전영진;서형석;변영환;이재우
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2007년도 제28회 춘계학술대회논문집
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    • pp.317-321
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    • 2007
  • PSP는 Pressure Sensitive Paint의 약자로 대기중의 산소량을 측정하여 전역적인 압력정보를 광학적으로 측정 할 수 있다. 본 연구에서는 PSP를 사용하여 jet injection 후류의 표면압력 분포를 알아보았다. 또한 Jet injection 5mm앞에 종횡비 1에서 4까지의 사각형 Cavity를 위치시켜 후류에 미치는 영향을 알아보았다. Jet injection 후류의 압력 분포는 Cavity의 전단층의 영향으로 Cavity가 없을 때와 비교해서 옆으로 넓게 퍼지면서 강도는 약해지는 모습을 보인다. 또한 Cavity의 종횡비가 커짐에 따라서 전단층의 크기가 커지고 그 영향이 커졌다. 측정된 압력은 압력공의 결과, CFD의 결과와 비교하였으며 근접한 값을 보였다.

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난류유동 해석을 위한 Dynamic PIV 시스템의 개발 (Development of a Dynamic PIV System for Turbulent Flow Analysis)

  • 이상준;장영길;김석
    • 한국가시화정보학회지
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    • 제3권1호
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    • pp.71-77
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    • 2005
  • Information on temporal evolution of whole velocity fields are essential for physical understanding of a complicated turbulent flow. Due to advances of high-speed imaging technique, laser and electronics, high-speed digital cameras and high-repetition pulse lasers are commercially available in nowadays. A dynamic PIV system that can measure consecutive instantaneous velocity field with 1K$\times$ 1K pixels resolution at 1 fps was developed. It consists of a high-speed CMOS camera and a high-repetition Nd:YLF pulse laser. Theoretically, it can capture velocity fields at 20 fps with a reduced spatial resolution. In order to validate its performance, the dynamic PIV system was applied to a turbulent jet of which Reynolds number is about 3000. The particle images of 1024$\times$512 pixels were captured at a sampling rate of 4 KHz. The dynamic PIV system measured successfully the temporal evolution of instantaneous velocity fields of the turbulent jet, from which spectral analysis of turbulent structure was also feasible.

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대퇴-대퇴동맥 우회 인조혈관 폐색에서 AngioJet Rheolytic Thrombectomy System과 색전보호기구를 이용한 혈전제거술: 증례 보고 (Thrombectomy of Femoro-Femoral Bypass Graft Occlusion Using the AngioJet Rheolytic Thrombectomy System and Embolic Protection Device: A Case Report)

  • 강한솔;이상준;송순영;김응태;고성은;박성민
    • 대한영상의학회지
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    • 제82권2호
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    • pp.447-454
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    • 2021
  • 저자들은 대퇴-대퇴동맥 우회 인조혈관 폐색 환자에서 AngioJet Rheolytic Thrombectomy System (이하 AngioJet)과 색전보호기구를 이용하여 성공적으로 혈전제거술을 시행한 1예를 보고하고자 한다. 하지 혈관 전산화단층촬영에서 좌측에서 우측으로의 대퇴-대퇴 우회 인조혈관 폐색 소견을 보였다. AngioJet을 이용한 흐름 용해 혈전제거술과 풍선 혈관성형술을 시행하여 우측 하지 혈류를 재개통 시켰으며, 시술 중 우측 표재성 대퇴동맥에 색전보호기구를 거치시켜 효과적으로 원위부 색전을 예방할 수 있었다.

연령에 따른 비행시차 후의 수면-각성주기 변화 (The Changes of Sleep-Wake Cycle from Jet-Lag by Age)

  • 김인;이승환;서광윤
    • 수면정신생리
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    • 제3권2호
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    • pp.18-31
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    • 1996
  • Jet-lag can be defined as the cumulative physiological and psychological effects of rapid air travel across multiple time zones. Many reports have suggested that age-related changes in sleep reflect fundamental changes in the circadian system and in significant declines in slow wave sleep. Jet lag is a dramatic situation in which the changes of the phase of circadian process and homeostatic process of sleep occur. Thus the authors evaluatead the changes of sleep-wake cycle from jet lag by age. Thirty-eight healthy travellers were studied for 3 days before and 7 days after jet-flights across seven to ten time zone. They were aged 19-70, They trareled eastbound, Seoul to North America (USA, Canada). Sleep onset time, wake-up time, sleep latency, awakening frequency on night sleep, awakening duration on night sleep, sleepiness at wake-up and nap length were evaluated. Our results suggest that by the 7 to 10 time zone shift, the old age group was significantly influenced in sleep-wake cycles. The date on which subjective physical condition was recovered was $6.23{\pm}83$ day after arrivals for old age group, while for young and middle age group, $4.46{\pm}1.50$ day and $4.83{\pm}1.52$ day, respectively. In old age group, sleep onset time was later than baselines and could not recover untill 7th day. But in other groups, the recovery was within 5th day. Nap dura fion was longer in old age group through jet lag than younger age group. In other parameters, there was no definite difference among three age groups. Our results suggested that the old age was significantly influenced by the disharmony between internal body clock and sleep-wake cycle needed at the travel site. Thus we proved that recovery ability from jet lag was age-dependent as well as travelling direction-dependent. To demonstrate more definite evidence, EEG monitoring and staging of sleep were funthun encouraged.

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150마력급 선내형 소형 워터제트 추진시스템 개발 (The development of small water-jet propulsion for 150HP grade inboard type)

  • 이중섭;이치우
    • Journal of Advanced Marine Engineering and Technology
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    • 제38권3호
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    • pp.246-252
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    • 2014
  • 본논문은 150마력급 선내형 소형 워터제트 추진시스템 개발에 대한 연구이다. 워터제트는 흡입부, 임펠러, 디퓨저(공기확산기), 후진부와 메인 샤프트로 구성되어 있다. 워터제트의 구성품은 사형 주조후 정밀가공을 거쳐 개발하였다. 워터제트 추진기관의 개발은 각각의 부품에 대한 설계-제작-검사의 과정을 거쳐 최종 완성하였으며, 육상 시험 풀에서는 선체의 이동 없이 워터제트의 펌프 특성을 확인한 결과, 최대 37m/s의 유속과 0.29m3/s의 유량을 배출할 수 있는 성능을 확보하였다. 본 연구에서 개발된 워터제트 추진장치를 설치한 21ft 시험선을 사용하여 실증 연구를 수행하였다. 그 결과, 국내 연안에서 시험시 선체무게와 엔진등 기타 부수적인 무게가 대략 1.2ton 가량 이였으며 이 상태에서 엔진회전수 3,700rpm에서 최대시속 45km/h의 운항속도를 기록하였다.

Semi-batch Jet Loop Reactor에서 연소 배가스중 CO2를 이용한 알칼리 폐수 중화 (Neutralization of Synthetic Alkaline Wastewater with CO2 in a Semi-batch Jet Loop Reactor)

  • 손민기;성호진;이제근
    • 한국연소학회지
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    • 제18권2호
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    • pp.17-22
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    • 2013
  • In this study, we tested the absorption of $CO_2$ in combustion gas into an alkaline wastewater to simultaneously control $CO_2$ and wastewater. During the experiment, we investigated the effects of operating parameters on neutralization characteristics of the wastewater by using $CO_2$ in a bench-scale semi-batch jet loop reactor (0.1 m diameter and 1.0 m in height). The operating parameters investigated in the study are gas flow rate of 1.0-2.0 L/min, liquid recirculation flow rate of 4-32 L/min, and liquid temperature of $20-25^{\circ}C$. It was shown that the initial pH of wastewater rapidly decreased with increased gas flow rate for a given liquid recirculation flow rate. This was due to the increase in the gas holdup and the interfacial area at higher gas flow rate in the reactor. At constant gas flow rate, the time required to neutralize the wastewater initial pH of 10.1 decreased with liquid recirculation flow rate ($Q_L$), reached a minimum value in the range of $Q_L$ = 16-24 L/min, and then increased with further increase in $Q_L$. Further, the time required to neutralize the wastewater was shortened at higher temperatures.