• Journal of Mechanical Science and Technology
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• 제18권10호
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• pp.1819-1828
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• 2004

The purpose of this paper is to investigate the effects of slits and swirl vanes on the turbulence augmentation in the flow fields of a gun-type gas burner using an X-type hot-wire probe. The gun-type gas burner adopted in this study is composed of eight slits and swirl vanes located on the surface of an inclined baffle plate. Experiment was carried out at a flow rate of 450 ι/min in burner model installed in the test section of subsonic wind tunnel. Swirl vanes playa role diffusing main flow more remarkably toward the radial direction than axial one, but slits show a reverse feature. Consequently, both slits and swirl vanes remarkably increase turbulence intensity in the whole range of a gun-type gas burner with a cone-type baffle plate.

• Nuclear Engineering and Technology
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• 제54권5호
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• pp.1890-1901
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• 2022

We have assessed the applicability of the thermal-hydraulic system analysis code, SPACE, to a small modular reactor called SMART. For the assessment, the experimental data from a scale-down integral-test facility, SMART-ITL, were used. It was conformed that the SPACE code unrealistically calculates the safety injection flow rate through the CMT and SIT during a small-break loss-of-coolant experiment. This unrealistic behavior was due to the overprediction of interfacial heat transfer at the steam-water interface in a vertically stratified flow in the tanks. In this study, a special thermal-hydraulic component model has been developed to realistically calculate the interfacial heat transfer when a strong non-equilibrium two-phase flow is formed in the CMT or SIT. Additionally, we developed a special heat structure model, which analytically calculates the heat transfer from the hot steam to the cold tank wall. The combination of two models for the tank are called the special component model. We assessed it using the SMART-ITL passive safety injection system (PSIS) test data. The results showed that the special component model well predicts the transient behaviors of the CMT and SIT.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2009년도 제33회 추계학술대회논문집
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• pp.97-100
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• 2009

한국형 발사체용 액체로켓엔진을 개발하기 위한 75톤급 연소기 기술검증 시제를 제작하여 수류시험 및 점화시험을 수행하였다. 기존의 연소기에 새롭게 도입된 기술인 점화, 막냉각, 산화제 선공급방식을 반영하기 위해 시험설비를 수정 및 개량하였다. 산화제 및 연료 수류시험을 통해 공급라인, 점화기 라인, 연소기의 수력학적 특성, 추진제 충전시간을 파악하여 점화순서를 결정하였다. 점화 cyclogram을 통해 점화기의 점화시험을 성공적으로 수행하였으며, 향후 연소시험을 위한 기초 자료를 습득하였다.

• Nuclear Engineering and Technology
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• 제28권4호
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• pp.405-414
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• 1996

In this paper, the unsteady 2-dimensional turbulent flow model for thermal stratification in a pressurizer surge line of PWR plant is proposed to numerically investigate the heat transfer and flow characteristics. The turbulence model is adapted to the low Reynolds number K-$\varepsilon$ model (Davidson model). The dimensionless governing equations are solved by using the SIMPLE (Semi-Implicit Method for Pressure Linked Equations) algorithm. The results are compared with simulated experimental results of TEMR Test. The time-dependent temperature profiles in the fluid and pipe nil are shown with the thermal stratification occurring in the horizontal section of the pipe. The corresponding thermal stresses are also presented. The numerical result for thermal stratification by the outsurge during heatup operation of PWR shows that the maximum dimensionless temperature difference is about 0.83 between hot and cold sections of pipe well and the maximum thermal stress is calculated about 322MPa at the dimensionless time 28.5 under given conditions.

• 대한기계학회논문집B
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• 제27권4호
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• pp.466-475
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• 2003

The gun-type gas burner adopted in this study is generally composed of eight slits and swirl vanes. Thus, this paper is studied to investigate the effect of slits and swirl vanes on the turbulent flow fields in the horizontal plane of gas swirl burner with a cone type baffle plate measured by using X-probe from hot-wire anemometer system. This experiment is carried out at flow rate 450 $\ell$/min in the test section of subsonic wind tunnel. The axial mean velocity component in the case of burner model with only swirl vanes shows the characteristic that spreads more remarkably toward the radial direction than axial one, it does, however, directly opposite tendency in the case of burner model with only slits. Consequently. both slits and swirl vanes composing of gun-type gas burner play an important role in decrease of the speed near slits and increase of the flow speed in the central part of a burner because the biggest speed spurted from slits encircles rotational flow by swirl vanes and it drives main flow toward the axial direction. Moreover, the turbulent intensities and turbulent kinetic energy of gun-type gas burner are distributed with a fairly bigger size within X/R<0.6410 than burner models which have only slits or swirl vanes because the rotational flow by swirl vanes and the fast jet flow by slits increase flow mixing, diffusion, and mean velocity gradient effectively.

• 한국소성가공학회:학술대회논문집
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• 한국소성가공학회 2009년도 춘계학술대회 논문집
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• pp.417-420
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• 2009

The hot forming process of a CAM for vessel engine was designed by finite element (FE) simulation and experimental analysis. An aim of process design was to achieve the near-net shaped CAM forgings by hot forging process. Based on the compression test results of the low alloy steel, deformation processing map was generated using the superposition approach between the dynamic materials model (DMM) and flow stability and/or instability criteria. From the processing map, the initial heating temperature was determined as $1200^{\circ}C$. FE analysis was simulated to predict the formation of rolling defects and deformed shape with different forging designs. Optimum process design suggested in this work was made by comparing with the CAM for vessel engine manufactured by actual forging process.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2007년도 제29회 추계학술대회논문집
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• pp.31-34
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• 2007

본 연구는 고온의 연소 가스를 이용하여 고공 환경 모사용 초음속 디퓨저의 성능을 파악하는 것이다. 실험 장치는 크게 액체로켓 연소실, 진공 챔버, 냉각수 링 및 디퓨저로 구성되어 있다. 먼저 연소실험 전에 고압의 질소가스(30barg)와 진공 펌프를 이용하여 액체로켓 엔진과 디퓨저의 기밀시험을 수행 하였다. 제작된 디퓨저를 포함한 시험 리그의 기밀테스트 결과， 고압 조건 및 진공압 조건에서 모두 누설이 없이 양호하였다.

• 한국산업정보학회논문지
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• 제28권6호
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• pp.21-27
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• 2023

현대 함정은 외부로 방사되는 적외선 신호를 낮추기 위해 폐기관에 적외선 신호저감 장치(Infra-Red Signature Suppression system, IRSS)를 설치한다. 그리고 함정은 생의 주기가 매우 긴 전략 자산으로 탑재 장비들의 성능에 대한 높은 신뢰성을 충분히 확보해야 한다. 따라서, IRSS와 같은 장비들은 설계 단계에서 모형시험을 통해 성능평가를 하고 있다. IRSS의 모형시험에서는 다양한 계측기기들이 사용된다. 그러므로, 모형시험 단계 이전에 계측기들의 신뢰성을 평가해야 한다. 본 연구에서는 IRSS 모형시험에 사용되는 계측 장비들의 신뢰성 평가에 관한 연구를 수행하였다. 시험 장비와 계측기는 열 풍동 시험기, 피토 튜브와 디지털 차압계, 열전대 센서 그리고 디지털 기록계가 사용되었다. 계측 결과 열 풍동 시험기의 풍속이 증가할수록 유동의 계측 편차가 감소하였으며, 열전대 센서의 온도는 사용 방법에 따라 반응 속도 및 민감도의 차이를 보였다.

• 한국항공우주학회지
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• 제45권2호
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• pp.85-91
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• 2017

본 연구에서는 NREL 5 MW 해상풍력터빈 모형의 후류 유동장 분석을 위해 1/86 축소모형을 사용한 실험적 연구를 수행하였다. 정격출력 속도 11.4 m/s와 회전수 1,045 rpm 조건에서 열선풍속계를 사용하여 반경의 6배까지 후류에서 속도 결핍 및 난류도 변화를 측정하는 풍동시험을 수행하였다. 그 결과 풍력터빈의 후류에서의 속도결핍은 횡방향과 수직 방향으로는 반경의 2배 이내에서 회복됨을 볼 수 있었으며, 끝단 와류에 의한 영향은 반경의 5배 이후에는 나타나지 않음을 볼 수 있었다. 또한, 후류의 난류도는 블레이드 끝단 부근에서 크게 나타나며 길이방향으로 반경 거리까지는 급격한 감소가 일어나지만 이 이후부터 반경의 6배까지 유지되었다.

• 제어로봇시스템학회논문지
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• 제7권7호
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• pp.567-573
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• 2001

A real-time HVAC system is proposed which implements real-time control of thermal environment for virtual reality. It consists of a pair of hot and cold loops that serve as thermal reservoirs, and a mixing box to mix hot and cold air streams flowing if from loops. Their flow rates are controlled in real-time to meet a set temperature and flow rate. A cascade control algorithm along with gain scheduling is applied to the system and test results shows that the closed-loop response approached set values within 3 to 4 seconds.