• 제목/요약/키워드: Hot Channel Analysis

검색결과 68건 처리시간 0.021초

평면 난류 오프셋 제트에 관한 연구 (A Study on the Plane Turbulent Offset Jet)

  • 유정열;강신형;채승기;좌성훈
    • 대한기계학회논문집
    • /
    • 제10권3호
    • /
    • pp.357-366
    • /
    • 1986
  • 본 연구에서는 3공피토우관 및 열선유속계를 사용하여 벽에 평행한 2차원 난류제트의 난류량들을 측정하였고, 스캐니 밸브를 이용하여 벽면아력분포를 측정함 으로써 재순환 영역을 포함한 전체유동장에서의 유동특성을 고찰하였다. 또한 잘 알려진 표준 k-.epsilon. 난류모형 및 유선곡률을 고려한 수정된 k-.epsilon. 난류모형을 이용하여 측정 수치해석을 수행하였다.

Conceptual design of a high neutron flux research reactor core with low enriched uranium fuel and low plutonium production

  • Rahimi, Ghasem;Nematollahi, MohammadReza;Hadad, Kamal;Rabiee, Ataollah
    • Nuclear Engineering and Technology
    • /
    • 제52권3호
    • /
    • pp.499-507
    • /
    • 2020
  • Research reactors for radioisotope production, fuel and material testing and research activities are designed, constructed and operated based on the society's needs. In this study, neutronic and thermal hydraulic design of a high neutron flux research reactor core for radioisotope production is presented. Main parameters including core excess reactivity, reactivity variations, power and flux distribution during the cycle, axial and radial power peaking factors (PPF), Pu239 production and minimum DNBR are calculated by nuclear deterministic codes. Core calculations performed by deterministic codes are validated with Monte Carlo code. Comparison of the neutronic parameters obtained from deterministic and Monte Carlo codes indicates good agreement. Finally, subchannel analysis performed for the hot channel to evaluate the maximum fuel and clad temperatures. The results show that the average thermal neutron flux at the beginning of cycle (BOC) is 1.0811 × 1014 n/㎠-s and at the end of cycle (EOC) is 1.229 × 1014 n/㎠-s. Total Plutonium (Pu239) production at the EOC evaluated to be 0.9487 Kg with 83.64% grade when LEU (UO2 with 3.7% enrichment) used as fuel. This designed reactor which uses LEU fuel and has high neutron flux and low plutonium production could be used for peaceful nuclear activities based on nuclear non-proliferation treaty concepts.

이기종 무선 환경에서 Load sharing을 이용한 Soft Load Balancing 기술 (Soft Load Balancing Using the Load Sharing Over Heterogeneous Wireless Networks)

  • 손혁민;이상훈;김수창;신연승
    • 한국통신학회논문지
    • /
    • 제33권7A호
    • /
    • pp.757-767
    • /
    • 2008
  • 차세대 이동 통신망의 발전으로 상용 망과 이 기종 망이 서로 겹쳐진 다중 망 구조가 형성될 것이다. 이러한 여러 망이 겹쳐진 다중 망 구조에서 전체 무선자원의 사용 효율을 높이고 Eb/Io (bit energy-to-interference plus noise density ratio)를 개선하기 위해 이기종망간 혹은 동종망간 상호 연동 기술이 필요하다. 본 논문에서는 이러한 동종망과 이기종망들이 서로 겹쳐져 있는 다중 셀 환경에서 load를 효율적으로 분산시킴으로써 무선 자원의 효율을 높이고 신호의 간섭양을 줄여 사용자의 QoS 보장 및 성능 개선을 위한 soft load balancing algorithm을 제안 및 분석한다. 본 논문에서는 수학적 분석을 통해 효율적인 load sharing을 위한 최적의 LBR (load balancing ratio) 을 구하고 이를 이용하여 각 network에 traffic 양을 할당하여 서비스한다. 그러므로 soft load balancing 알고리듬은 보다 안정적인 데이터 전송을 가능하게 한다.

온라인 컴퓨터 시스템에 의한 실린더내 충돌분류의 통계학적 난류특성 연구 (Study on the statistical turbulence characteristics of cross jets in the cylinder by on-line computer system)

  • 노병준;박종호
    • 대한기계학회논문집
    • /
    • 제12권4호
    • /
    • pp.876-891
    • /
    • 1988
  • 본 연구에서는 실린더내의 혼합유동을 고찰하기 위하여 두 분류를 충동 유동 시켜 충돌 후 혼합 유동 상태를 온라인 측정 시스템에 의하여 계측하였다.실린더내 의 난류에 의한 혼합현상을 구명하기 위하여 혼합영역을 중심으로 3차원유동 성분들의 평균속도, 난류응력 등을 측정하여 일반 자유분류의 반실험식과 비교 검토하였으며, 본 실험 결과에 잘 일치하는 반실험식을 가정식으로부터 컴퓨터에 의한 점근적 방법으 로 구하였다.

난류충돌유동의 질량유량비에 따른 혼합유동구조에 관한 실험적 연구 (An Experimental Study on the Mixing Flow Structure of Turbulent Cross Flow with Respect to the Ratio of Mass Flow Rate)

  • 이대옥;노병준
    • 대한기계학회논문집
    • /
    • 제16권11호
    • /
    • pp.2150-2158
    • /
    • 1992
  • 본 연구에서는 복잡한 유동형태를 지닌 충돌분사류에 대한 유동특성을 연구하 기 위하여 단순화된 실험모델로써 형상이 동일한 두 원형분류의 충돌에 의한 충돌분류 의 혼합현상 및 유동구조 등을 질량유량비의 변화에 따라 유체역학적으로 구명하고자 하였으며, 본 연구 결과는 연소기관에서의 연소효율 증대 및 구조개선등의 공학적 응 용을 위한 기본자료로 활용하고, 이론적 연구에 의한 난류의 유동구조 및 유동특성 에 대한 타당성 입증과 이론적 모델의 보완을 위한 실험자료로 이용하고자 한다. 충돌유동에 영향을 미치는 주요인자는 노즐직경, 충돌각, 충돌질량유량비, 온도, 밀도 등이며, 이 인자들 중에서 충돌질량유량비와 출돌각이 충돌후 형성되는 난류혼합유동 에 지배적인 영향을 미치므로, 본 연구에서는 두 원형분류의 충돌질량유량비를 가변할 수 있는 장치를 고안하였으며, 두 분류의 충돌각을 45˚로 고정하고, 고속측과 저속측 노즐의 질량유량비를 1.0, 0.8, 0.6, 0.4로 설정하여 질량유량비에 따른 혼합 유동구 조의 구명을 위한 실험적인 연구를 수행하였다. 충돌후의 혼합유동의 특성을 연구하 기 위하여 유동중심궤적, 유동반폭, 유동단면, 2차원 및 3차원 유동장, 평균속도분포 등을 온라인 컴퓨터시스템을 이용하여 측정분석하였다.

설비공학 분야의 최근 연구 동향 : 2012년 학회지 논문에 대한 종합적 고찰 (Recent Progress in Air-Conditioning and Refrigeration Research : A Review of Papers Published in the Korean Journal of Air-Conditioning and Refrigeration Engineering in 2012)

  • 한화택;이대영;김사량;김현정;최종민;박준석;김수민
    • 설비공학논문집
    • /
    • 제25권6호
    • /
    • pp.346-361
    • /
    • 2013
  • This article reviews the papers published in the Korean Journal of Air-Conditioning and Refrigeration Engineering during 2012. It is intended to understand the status of current research in the areas of heating, cooling, ventilation, sanitation, and indoor environments of buildings and plant facilities. The conclusions are as follows : (1) The research works on thermal and fluid engineering have been reviewed as groups of fluid machinery, pipes and valves, fuel cells and power plants, ground-coupled heat pumps, and general heat and mass transfer systems. Research issues are mainly focused on new and renewable energy systems, such as fuel cells, ocean thermal energy conversion power plants, and ground-coupled heat pump systems. (2) Research works on the heat transfer area have been reviewed in the categories of heat transfer characteristics, pool boiling and condensing heat transfer, and industrial heat exchangers. Researches on heat transfer characteristics included the results for natural convection in a square enclosure with two hot circular cylinders, non-uniform grooved tube considering tube expansion, single-tube annular baffle system, broadcasting LED light with ion wind generator, mechanical property and microstructure of SA213 P92 boiler pipe steel, and flat plate using multiple tripping wires. In the area of pool boiling and condensing heat transfer, researches on the design of a micro-channel heat exchanger for a heat pump, numerical simulation of a heat pump evaporator considering the pressure drop in the distributor and capillary tubes, critical heat flux on a thermoexcel-E enhanced surface, and the performance of a fin-and-tube condenser with non-uniform air distribution and different tube types were actively carried out. In the area of industrial heat exchangers, researches on a plate heat exchanger type dehumidifier, fin-tube heat exchanger, an electric circuit transient analogy model in a vertical closed loop ground heat exchanger, heat transfer characteristics of a double skin window for plant factory, a regenerative heat exchanger depending on its porous structure, and various types of plate heat exchangers were performed. (3) In the field of refrigeration, various studies were executed to improve refrigeration system performance, and to evaluate the applicability of alternative refrigerants and new components. Various topics were presented in the area of refrigeration cycle. Research issues mainly focused on the enhancement of the system performance. In the alternative refrigerant area, studies on CO2, R32/R152a mixture, and R1234yf were performed. Studies on the design and performance analysis of various compressors and evaporator were executed. (4) In building mechanical system research fields, twenty-nine studies were conducted to achieve effective design of mechanical systems, and also to maximize the energy efficiency of buildings. The topics of the studies included heating and cooling, HVAC system, ventilation, renewable energy systems, and lighting systems in buildings. New designs and performance tests using numerical methods and experiments provide useful information and key data, which can improve the energy efficiency of buildings. (5) In the fields of the architectural environment, studies for various purposes, such as indoor environment, building energy, and renewable energy were performed. In particular, building energy-related researches and renewable energy systems have been mainly studied, reflecting interests in global climate change, and efforts to reduce building energy consumption by government and architectural specialists. In addition, many researches have been conducted regarding indoor environments.

초기 시청시간 패턴 분석을 통한 대흥행 드라마 예측 (Prediction of a hit drama with a pattern analysis on early viewing ratings)

  • 남기환;성노윤
    • 지능정보연구
    • /
    • 제24권4호
    • /
    • pp.33-49
    • /
    • 2018
  • TV 드라마는 타 장르에 비해 시청률과 채널 홍보 효과가 매우 크며, 한류를 통해 산업적 효과와 문화적 영향력을 확인시켜줬다. 따라서, 이와 같은 드라마의 흥행 여부를 예측하는 일은 방송 관련 산업에서 매우 중요한 부분임은 주지의 사실이다. 이를 위해서 본 연구에서는 2003년부터 2012년까지 10년간, 지상파 채널을 통해 방송된, 총 280개의 TV 미니시리즈 드라마를 분석하였다. 이들 드라마 중 평균 시청률 상위 45개, 하위 시청률 45개를 선정하여 흥행 드라마의 시청시간 분포 (5%~100%, 11-Step) 모형을 만들었다. 이들 기준 모형과 신규 드라마의 시청시간 분포와의 이격 거리를 Euclidean/Correlation으로 측정한 유사도(Similarity)를 통해, 시청자의 초기(1~5회) 시청시간 분포로 신규 드라마의 성패 여부를 예측하는 모델을 만들었다. 또한 총 방송 시간 중 70% 이상 시청한 시청자를 열혈 시청층(이하 열혈층) 으로 분류하고, 상위/하위 드라마의 평균값과 비교하여, 신규 드라마의 흥행여부를 판별할 수 있도록 설계하였다. 연구 결과 드라마의 초반 시청자 충성도(시청시간)는 드라마의 대흥행 여부를 예측하는데 중요한 요소임을 밝혔으며, 최대 75.47%의 확률로 대흥행 드라마의 탄생을 예측할 수 있었다.

공동이 있는 수직 분사 초음속 연소기 내의 불안정 연소유동 해석 (Numerical Analysis of Unstable Combustion Flows in Normal Injection Supersonic Combustor with a Cavity)

  • Jeong-Yeol Choi;Vigor Yang
    • 한국추진공학회:학술대회논문집
    • /
    • 한국추진공학회 2003년도 제20회 춘계학술대회 논문집
    • /
    • pp.91-93
    • /
    • 2003
  • A comprehensive numerical study is carried out to investigate for the understanding of the flow evolution and flame development in a supersonic combustor with normal injection of ncumally injecting hydrogen in airsupersonic flows. The formulation treats the complete conservation equations of mass, momentum, energy, and species concentration for a multi-component chemically reacting system. For the numerical simulation of supersonic combustion, multi-species Navier-Stokes equations and detailed chemistry of H2-Air is considered. It also accommodates a finite-rate chemical kinetics mechanism of hydrogen-air combustion GRI-Mech. 2.11[1], which consists of nine species and twenty-five reaction steps. Turbulence closure is achieved by means of a k-two-equation model (2). The governing equations are spatially discretized using a finite-volume approach, and temporally integrated by means of a second-order accurate implicit scheme (3-5).The supersonic combustor consists of a flat channel of 10 cm height and a fuel-injection slit of 0.1 cm width located at 10 cm downstream of the inlet. A cavity of 5 cm height and 20 cm width is installed at 15 cm downstream of the injection slit. A total of 936160 grids are used for the main-combustor flow passage, and 159161 grids for the cavity. The grids are clustered in the flow direction near the fuel injector and cavity, as well as in the vertical direction near the bottom wall. The no-slip and adiabatic conditions are assumed throughout the entire wall boundary. As a specific example, the inflow Mach number is assumed to be 3, and the temperature and pressure are 600 K and 0.1 MPa, respectively. Gaseous hydrogen at a temperature of 151.5 K is injected normal to the wall from a choked injector.A series of calculations were carried out by varying the fuel injection pressure from 0.5 to 1.5MPa. This amounts to changing the fuel mass flow rate or the overall equivalence ratio for different operating regimes. Figure 1 shows the instantaneous temperature fields in the supersonic combustor at four different conditions. The dark blue region represents the hot burned gases. At the fuel injection pressure of 0.5 MPa, the flame is stably anchored, but the flow field exhibits a high-amplitude oscillation. At the fuel injection pressure of 1.0 MPa, the Mach reflection occurs ahead of the injector. The interaction between the incoming air and the injection flow becomes much more complex, and the fuel/air mixing is strongly enhanced. The Mach reflection oscillates and results in a strong fluctuation in the combustor wall pressure. At the fuel injection pressure of 1.5MPa, the flow inside the combustor becomes nearly choked and the Mach reflection is displaced forward. The leading shock wave moves slowly toward the inlet, and eventually causes the combustor-upstart due to the thermal choking. The cavity appears to play a secondary role in driving the flow unsteadiness, in spite of its influence on the fuel/air mixing and flame evolution. Further investigation is necessary on this issue. The present study features detailed resolution of the flow and flame dynamics in the combustor, which was not typically available in most of the previous works. In particular, the oscillatory flow characteristics are captured at a scale sufficient to identify the underlying physical mechanisms. Much of the flow unsteadiness is not related to the cavity, but rather to the intrinsic unsteadiness in the flowfield, as also shown experimentally by Ben-Yakar et al. [6], The interactions between the unsteady flow and flame evolution may cause a large excursion of flow oscillation. The work appears to be the first of its kind in the numerical study of combustion oscillations in a supersonic combustor, although a similar phenomenon was previously reported experimentally. A more comprehensive discussion will be given in the final paper presented at the colloquium.

  • PDF