• 제목/요약/키워드: Turbulence Penetration

검색결과 31건 처리시간 0.025초

정적챔버에서 분위기 압력에 따른 비증발 디젤분무특성 연구 (A Study on the Non-evaporating Diesel Spray Characteristics as a Function of Ambient Pressure in Constant Volume Combustion Chamber)

  • 전충환;정정훈;김현규;송주헌;장영준
    • Journal of Advanced Marine Engineering and Technology
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    • 제34권5호
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    • pp.645-652
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    • 2010
  • 본 연구의 목적은 다양한 분위기 압력 하에서 커먼레일 디젤인젝터를 통해 분사되는 비증발 디젤 분무특성에 관한 연구이다. 디젤분무의 거시적 특성으로 분무관통거리와 분무각을 음영사진과 이미지프로세싱으로 연구하였다. 수치해석은 상용 CFD프로그램인 AVL-FIRE를 사용하였다. 분열모델은 WAVE모델을 사용하였으며 표준 $k-{\varepsilon}$난류모델을 적용하였다. 분무각과 Zeuch법을 적용한 연료 분사율을 수치해석의 입력값으로 사용하였다. 분무관통거리를 실험값과 비교하여 좋은 결과를 얻었고 수치해석을 통하여 노즐팁 하류방향으로 분무의 각 구간별 액적입경분포를 알아보았다.

국내원전 배관계통 열성층 연구개발 현황 (Status of Thermal Stratification Research on Piping System in Korea Nuclear Power Plant)

  • 이선기
    • 한국압력기기공학회 논문집
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    • 제12권2호
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    • pp.25-33
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    • 2016
  • The thermal stratification phenomenon in the nuclear power plant can cause abnormal deformation of the piping, contact with the support, damage to the support system. Repetition of the thermal stratification phenomenon or variation of the thermal boundary layer can cause thermal fatigue. Thermal stratification phenomenon in nuclear power plants is still an ongoing issue and active research has been carried out. In this paper, the current situation in Korean nuclear power plants is described, followed by the status of research and the future problems on the thermal stratification phenomenon in Korea.

가스터빈 연소기 내 운전조건 변화에 따른 분무연소 특성 연구 (Study on Characteristics of Spray Combustion for Various Operation Conditions in a Gas Turbine Combustor)

  • 조상필;김호영;박심수
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2002년도 제24회 KOSCO SYMPOSIUM 논문집
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    • pp.3-10
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    • 2002
  • In this work, numerical parametric studies on spray combustion have been conducted. In simulation of turbulence, RNG ${\kappa}-{\varepsilon}model$ is adopted. Initial spray distribution is specified by Rosin-Rammler distribution function. Eddy break-up model is adopted as a combustion model. The parameters considered are inlet air temperature, swirl number, and SMD. With higher inlet air temperature, the axial velocities are increased and penetration of primary jet is stronger than that of lower inlet air temperature and temperature at the exit of combustor is more uniform. Combustion efficiency is improved with high inlet air temperature. The effect of swirl number on flow field is not significant. It affect only recirculation zone. So temperature at upstream of combustor is influenced. Combustion efficiency deteriorate as SMD of fuel spray increase.

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냉각 파일런 분사를 이용한 스크램제트 연소기 내 혼합증대 (Mixing Augmentation with Cooled Pylon Injection in Scramjet Combustor)

  • 이상현
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2009년도 제33회 추계학술대회논문집
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    • pp.594-597
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    • 2009
  • The mixing characteristics of pylon injection in a Scramjet combustor and effects of film cooling to protect pylon from air-heating. Three-dimensional Navier-Stokes equations with $k-{\omega}$ SST turbulence model were used. Fuel hydrogen and air were considered as coolants. There were remarkable improvements of penetration and mixing rate with the pylon injection. There also over-heating on the front surface of pylon without film cooling. The coolant injected parallel to the front surface of the pylon protect the pylon from over-heating.

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초음속 연소기에서의 혼합과 연소현상에 관한 수치해석 (Numerical Simulation of Mixing and Combustion in a Normal Injection of the Scramjet)

  • 문수연;이충원;손창현
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 추계학술대회논문집B
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    • pp.475-480
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    • 2001
  • The flowfield of transverse jet in a supersonic air stream subjected to shock wave turbulent boundary layer interactions is simulated numerically by Generalized Taylor Galerkin(GTG) finite element methods. Effects of turbulence are taken into account with a two-equation $(k-\varepsilon)$ model with a compressibility correction. Injection pressures and slot widths are varied in the present study. Pressure, separation extents, and penetration heights are compared with experimental data. Favorable comparisons with experimental measurements are demonstrated.

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화학반응이 있는 난류경계층과 충격파의 상호작용에 대한수치해석 (Numerical Simulation of Chemically Reacting Shock Wave-Turbulent Boundary Layer Interactions)

  • 문수연;이충원;손창현
    • 대한기계학회논문집B
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    • 제26권3호
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    • pp.375-383
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    • 2002
  • The flowfield of transverse jet in a supersonic air stream subjected to shock wave turbulent boundary layer interactions is simulated numerically by Generalized Taylor Galerkin(GTG) finite element methods. Effects of turbulence are taken into account with a two-equation (k-$\varepsilon$) model with a compressibility correction. Injection pressures and slot widths are varied in the present study. Pressure, separation extents, and penetration heights are compared with experimental data. Favorable comparisons with experimental measurements are demonstrated.

원전 비상 노심냉각계통 배관 열성층화 현상 규명을 위한 실험적 연구 (Experimental Research for Identification of Thermal Stratification Phenomena in The Nuclear Powerplant Emergency Core Coolant System(ECCS).)

  • 송도인;최영돈;박민수
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 추계학술대회논문집B
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    • pp.735-740
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    • 2001
  • In the nuclear power plant, emergency core coolant system(ECCS) is furnished at reactor coolant system(RCS) in order to cool down high temperature water in case of emergency. However, in this coolant system, it occurs thermal stratification phenomena in case that there is the mixing of cooling water and high temperature water due to valve leakage in ECCS. This thermal stratification phenomena raises excessive thermal stresses at pipe wall. Therefore, this phenomena causes the accident that reactor coolant flows in reactor containment in the nuclear power plant due to the deformation of pipe and thermal fatigue crack(TFC) at the pipe wall around the place that it exists. Hence, in order to fundamental identification of this phenomena, it requires the experimental research of modeling test in the pipe flow that occurs thermal stratification phenomena. So, this paper models RCS and ECCS pipe arrangement and analyzes the mechanism of thermal stratification phenomena by measuring of temperature in variance with leakage flow rate in ECCS modeled pipe and Reynold number in RCS modeled pipe. Besides, results of this experiment is compared with computational analysis which is done in advance.

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냉각 파일런 분사를 이용한 스크램제트 연소기 내 혼합증대 (Mixing Augmentation with Cooled Pylon Injection in Scramjet Combustor)

  • 이상현
    • 한국추진공학회지
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    • 제14권1호
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    • pp.20-28
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    • 2010
  • 스크램제트 연소기 내 파일런 분사기의 연료-공기 혼합특성을 살펴보았으며, 공력가열로부터 파일런을 보호하기 위한 막냉각의 효과를 조사하였다. 수치연구를 위하여 3차원 Navier-Stokes 방정식과 $k-{\omega}$ SST 난류 모델을 이용하였다. 연료인 수소와 공기를 냉각 유체로 고려하였다. 파일런 분사기를 이용하는 경우 침투거리가 증대되고, 혼합률도 주목할 만큼 증대되었으나, 공력가열에 의한 파일런의 전방 표면 과열을 확인하였다. 파일런 전방에 파일런 표면에 평행한 냉각 제트를 분사하는 막냉각을 이용하면 파일런 표면의 과열을 막을 수 있음을 확인하였다.

DES를 이용한 초음속 유동내 수직 연료분사 유동의 비정상 3차원 해석 Part I : 비반응 유동장 (Unsteady Three-Dimensional Analysis of Transverse Fuel Injection into a Supersonic Crossflow using Detached Eddy Simulation Part I : Non-Reacting Flowfield)

  • 원수희;정인석;최정열
    • 한국항공우주학회지
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    • 제37권9호
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    • pp.863-878
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    • 2009
  • 초음속 주 유동내 연료의 수직분사에 따른 비정상 3차원 유동장을 DES 난류 모델을 이용해 모사하였다. 해석 결과는 시간에 따른 에디 거동 및 생성 빈도에 대해 실험과 비교되었으며, 에디 생성 메커니즘을 이해하기 위해 분사기 주변 와도에 대한 분석을 수행하였다. DES 난류 모델은 에디의 대류 특성을 비교적 정확하게 모사하고 있으나, 에디 생성빈도는 다소 과대 예측하고 있다. 분사기 상류 재순환 영역에서 엇회전하는 와류가 번갈아 떨어져 나가면서 에디 구조가 생성된다.

Numerical simulation of air discharged in subcooled water pool

  • Y. Cordova ;D. Blanco ;Y. Rivera;C. Berna ;J.L. Munoz-Cobo ;A. Escriva
    • Nuclear Engineering and Technology
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    • 제55권10호
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    • pp.3754-3767
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    • 2023
  • Turbulent jet discharges in subcooled water pools are essential for safety systems in nuclear power plants, specifically in the pressure suppression pool of boiling water reactors and In-containment Refueling Water Storage Tank of advanced pressurized water reactors. The gas and liquid flow in these systems is investigated using multiphase flow analysis. This field has been extensively examined using a combination of experiments, theoretical models, and Computational Fluid Dynamics (CFD) simulations. ANSYS CFX offers two approaches to model multiphase flow behavior. The non-homogeneous Eulerian-Eulerian Model has been used in this work; it computes global information and is more convenient to study interpenetrated fluids. This study utilized the Large Eddy Simulation Model as the turbulence model, as it is better suited for non-stationary and buoyant flows. The CFD results of this study were validated with experimental data and theoretical results previously obtained. The figures of merit dimensionless penetration length and the dimensionless buoyancy length show good agreement with the experimental measurements. Correlations for these variables were obtained as a function of dimensionless numbers to give generality using only initial boundary conditions. CFD numerical model developed in this research has the capability to simulate the behavior of non-condensable gases discharged in water.