• 한국추진공학회지
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• 제4권3호
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• pp.1-10
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• 2000

본 연구에서는 아음속/음속 이젝터의 성능을 평가하고, 공학적 설계를 위한 기초적 연구의 일환으로 일차원 기체역학 이론을 이용하여 이론해석을 수행하였다. 이론해석에서는 1차노즐의 유량계수, 디퓨저의 손실계수를 도입하여, 아음속/음속 이젝터의 목면적비, 유량비, 2차정체실의 압력 등을 이젝터 압축비의 함수로 도출하였다 본 연구에서 제시된 이론해석법은 아음속/음속 이젝터의 성능을 평가하는데 유용할 뿐만 아니라 이젝터 설계를 위한 자료로 활용될 수 있다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2006년도 제26회 춘계학술대회논문집
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• pp.331-336
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• 2006

초음속 터빈의 로터와 노즐사이의 간극은 터빈의 성능과 운전의 안정성에 직접적인 영향을 미치게 된다. 본 연구에서는 30톤급 개방형 액체로켓엔진용 터보펌프의 구동원으로 개발된 초음속 터빈에 대하여 노즐과 로터의 간극이 변화된 형상을 구현하고 이에 대한 계산을 수행한 후 그 결과를 분석하였다. 계산결과로부터 노즐-로터 간극이 증가함에 따라 이 영역에서의 전압력 손실이 증가하고 이에 따른 터빈 성능이 감소함을 확인하였다.

• 대한기계학회논문집B
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• 제30권12호
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• pp.1147-1154
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• 2006

An experimental investigation was conducted to enhance the heat/mass transfer for impingement/effusion cooling system when the initial crossflow was formed. For the improvement of heat transfer, the circular guide is installed on the injection hole. At the fixed jet Reynolds number of 10,000, the measurements were carried out for blowing ratios ranging from 0.5 to 1.5. The local heat/mass transfer coefficients on the effusion plate are measured using a naphthalene sublimation method. The result presents that the circular guide protects the injected jet from the initial crossflow, increasing the heat/mass transfer. The heat transfer of stagnation region is hardly changed regardless of the blowing ratio. The secondary peak is obviously formed by flow transition to turbulent flow. At high blowing ratio of 1.5, the circular guide produces $26{\sim}30%$ augmentation on the averaged heat/mass transfer while the case without circular guide leads to the low and non-uniform heat/mass transfer. With the increased heat/mass transfer, the installation of circular guide is accompanied by the increase of pressure loss in the channel. However, the pressure drop caused by the circular guide is lower than that for other cooling technique with the circular pin fin.

• 대한기계학회논문집B
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• 제20권10호
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• pp.3251-3261
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• 1996

Flows were measured in an unshrouded centrifugal impeller. By using a single slanted hot-wire probe and a Kiel probe mounted on the impeller hub disk, the 3-D relative velocities and the rotary stagnation pressures were measured in seven circumferential planes between the inlet and outlet of the impeller rotating at 700 rpm, which diameter is 0.39 meter, and the static pressures and the slip factor at the impeller outlet were estimated from the measured values. Measurements were made for three flow rates corresponding to zero incidence and two others with the greater and the smaller one than zero. From the measured data in these flow rates, the followings were investigated in the impeller passage, the variation of the primary and secondary flows, the leakage flows, the wake's position and its size, the static pressure rise and the loss production mechanism. Furthermore the static pressure and the slip factor were compared with the results of inviscid Quasi-3D calculation.

• Nuclear Engineering and Technology
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• 제39권4호
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• pp.257-272
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• 2007

Supercritical water-cooled reactors (SCWRs) are recognized as a Generation IV reactor concept. The Super LWR is a pressure-vessel type thermal spectrum SCWR with downward-flow water rods and is currently under study at the University of Tokyo. This paper reviews Super LWR safety. The fundamental requirement for the Super LWR, which has a once-through coolant cycle, is the core coolant flow rate rather than the coolant inventory. Key safety characteristics of the Super LWR inhere in the design features and have been identified through a series of safety analyses. Although loss-of-flow is the most important abnormality, fuel rod heat-up is mitigated by the "heat sink" and "water source" effects of the water rods. Response of the reactor power against pressurization events is mild due to a small change in the average coolant density and flow stagnation of the once-through coolant cycle. These mild responses against transients and also reactivity feedbacks provide good inherent safety against anticipated-transient-without-scram (ATWS) events without alternative actions. Initiation of an automatic depressurization system provides effective heat removal from the fuel rods. An "in-vessel accumulator" effect of the reactor vessel top dome enhances the fuel rod cooling. This effect enlarges the safety margin for large LOCA.

• 에너지공학
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• 제11권1호
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• pp.26-33
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• 2002

본 연구에서는 butterfly valve주위의 비압축성 및 압축성유동 특성을 수치해석을 통하여 조사하였다. 밸브는 문제를 단순화시키기 위하여 평판 디스크로 간주하였으며, 다양한 디스크 각도 및 압력비 변화에 대한 계산을 수행하였다. 각도가 증가함에 따라 디스크 상류면의 정체점은 디스크의 중심으로 이동하는 것을 볼 수 있었고, 입구공기의 유입 속도는 감소함을 볼 수 있었다. 최고 유속은 디스크와 벽면사이에 형성되는 vena contracta 효과에 의해 생기는 목의 하류에서 형성됨을 볼 수 있었다. 압력비를 감소함에 따라 압축성 효과는 증대되며 유동이 초음속화 되면서 생성되는 강한 wall jet에 의해 shock cell structure가 형성되는 것을 볼 수 있었다. 입구유량은 디스크 각도와 압력비의 증가에 따라서 감소하며, 압력손실계수는 디스크 각도의 증가 및 압력비의 감소에 따라 증가하였다.

• 한국환경과학회지
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• 제26권5호
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• pp.621-638
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• 2017

Meteorological characteristics related to variations in ozone ($O_3$) concentrations in the Korean peninsula before, during, and after Typhoon Talas (1112) were analyzed using both observation data and numerical modeling. This case study takes into account a high $O_3$ episode (e.g., a daily maximum of ${\geq}90ppb$) without rainfall. Before the typhoon period, high $O_3$ concentrations in the study areas (e.g., Daejeon, Daegu, and Busan) resulted from the combined effects of stable atmospheric conditions with high temperature under a migratory anticyclone (including subsiding air), and wind convergence due to a change in direction caused by the typhoon. The $O_3$ concentrations during the typhoon period decreased around the study area due to very weak photochemical activity under increased cloud cover and active vertical dispersion under a low pressure system. However, the maximum $O_3$ concentrations during this period were somewhat high (similar to those in the normal period extraneous to the typhoon), possibly because of the relatively slow photochemical loss of $O_3$ by a $H_2O+O(^1D)$ reaction resulting from the low air temperature and low relative humidity. The lowest $O_3$ concentrations during the typhoon period were relatively high compared to the period before and after the typhoon, mainly due to the transport effect resulting from the strong nocturnal winds caused by the typhoon. In addition, the $O_3$ increase observed at night in Daegu and Busan was primarily caused by local wind conditions (e.g., mountain winds) and atmospheric stagnation in the wind convergence zone around inland mountains and valleys.