• Title/Summary/Keyword: CFD 모사

Search Result 215, Processing Time 0.023 seconds

Investigation of Turbulent Analysis Methods for CFD of Gas Dispersion Around a Building (건물주위의 가스 확산사고에 대한 CFD 난류 해석기법 검토)

  • Ko, Min Wook;Oh, Chang Bo;Han, Youn Shik;Do, Kyu Hyung
    • Fire Science and Engineering
    • /
    • v.29 no.5
    • /
    • pp.42-50
    • /
    • 2015
  • Three simulation approaches for turbulence were applied for the computation of propane dispersion in a simplified real-scale urban area with one building:, Large Eddy Simulation (LES), Detached Eddy Simulation (DES), and Unsteady Reynolds Averaged Navier-Stokes (RANS). The computations were performed using FLUENT 14, and the grid system was made with ICEM-CFD. The propane distribution depended on the prediction performance of the three simulation approaches for the eddy structure around the building. LES and DES showed relatively similar results for the eddy structure and propane distribution, while the RANS prediction of the propane distribution was unrealistic. RANS was found to be inappropriate for computation of the gas dispersion process due to poor prediction performance for the unsteady turbulence. Considering the computational results and cost, DES is believed to be the optimal choice for computation of the gas dispersion in a real-scale space.

Evaluation of Ground Thermal Conductivity by Performing In-Situ Thermal Response test (TRT) and CFD Back-Analysis (현장 열응답 시험(TRT)과 CFD 역해석을 통한 지반의 열전도도 평가)

  • Park, Moonseo;Lee, Chulho;Park, Sangwoo;Sohn, Byonghu;Choi, Hangseok
    • Journal of the Korean Geotechnical Society
    • /
    • v.28 no.12
    • /
    • pp.5-15
    • /
    • 2012
  • In this study, a series of CFD (Computational Fluid Dynamics) numerical analyses were performed in order to evaluate the thermal performance of six full-scale closed-loop vertical ground heat exchangers constructed in a test bed located in Wonju. The circulation HDPE pipe, borehole and surrounding ground formation were modeled using FLUENT, a finite-volume method (FVM) program, for analyzing the heat transfer process of the system. Two user-defined functions (UDFs) accounting for the difference in the temperatures of the circulating inflow and outflow fluid and the variation of the surrounding ground temperature with depth were adopted in the FLUENT model. The relevant thermal properties of materials measured in laboratory were used in the numerical analyses to compare the thermal efficiency of various types of the heat exchangers installed in the test bed. The simulation results provide a verification for the in-situ thermal response test (TRT) data. The CFD numerical back-analysis with the ground thermal conductivity of 4 W/mK yielded better agreement with the in-situ thermal response tests than with the ground thermal conductivity of 3 W/mK.

Numerical Simulation on the ULPU-V Experiments using RPI Model (RPI모형을 이용한 ULPU-V시험의 수치모사)

  • Suh, Jungsoo;Ha, Huiun
    • Journal of the Korean Society of Safety
    • /
    • v.32 no.2
    • /
    • pp.147-152
    • /
    • 2017
  • The external reactor vessel cooling (ERVC) is well known strategy to mitigate a severe accident at which nuclear fuel inside the reactor vessel is molten. In order to compare the heat removal capacity of ERVC between the nuclear reactor designs quantitatively, numerical method is often used. However, the study for ERVC using computational fluid dynamics (CFD) is still quite scarce. As a validation study on the numerical prediction for ERVC using CFD, the subcooled boiling flow and natural circulation of coolant at the ULPU-V experiment was simulated. The commercially available CFD software ANSYS-CFX was used. Shear stress transport (SST) model and RPI model were used for turbulence closure and wall-boiling, respectively. The averaged flow velocities in the downcomer and the baffle entry under the reactor vessel lower plenum are in good agreement with the available experimental data and recent computational results. Steam generated from the heated wall condenses rapidly and coolant flows maintains single-phase flow until coolant boils again by flashing process due to the decrease of saturation temperature induced by higher elevation. Hence, the flow rate of coolant natural circulation does not vary significantly with the change of heat flux applied at the reactor vessel, which is also consistent with the previous literatures.

Assessment of MARS Multi-dimensional Two-phase Turbulent Flow Models for the Nuclear System Analysis (발전소 계통해석을 위한 MARS 코드의 다차원 이상 난류 유동 모델 검증계산)

  • Lee S.M.;Lee U.C.;Bae S.W.;Chung B.D.
    • Journal of Energy Engineering
    • /
    • v.15 no.1 s.45
    • /
    • pp.1-7
    • /
    • 2006
  • The multi-dimensional two-phase flow models were developed for analyze the multi-dimensional behaviors or nuclear systems. To verify the simple turbulence model, The single phase mixing problem in a rectangular slab was calculated and compared with the commercial CFD code results. That result shows a good agreement with the CFD result. And the RPI Air-water experiments were simulated to assess the two-phase turbulence model in the multi-dimensional component. The first calculated distribution or void-fraction is highly dispersed and diffusive. It was revealed that the main reason is undesirable stratification force in a horizontal stratified flow regimes. Therefore the horizontally stratified flow regime is deleted because the stratified flow regime is not expected in multi-dimensional flow. With the modification of the flow regime, the predicted flow patterns and void fraction profiles are in good agreement with the measured data.

Numerical investigation of blade tip vortex cavitation noise using Reynolds-averaged Navier-Stokes simulation and bubble dynamics model (Reynolds-averaged Navier-Stokes 해석과 기포동역학 모델을 이용한 날개 끝 와류 공동 소음의 수치적 고찰)

  • Ku, Garam;Cheong, Cheolung;Seol, Hanshin
    • The Journal of the Acoustical Society of Korea
    • /
    • v.39 no.2
    • /
    • pp.77-86
    • /
    • 2020
  • In this study, the Eulerian/Lagrangian one-way coupling method is proposed to predict flow noise due to Blade-Tip Vortex Cavitation (BTVC). The proposed method consists of four sequential steps: flow field simulation using Computational Fluid Dynamics (CFD) techniques, reconstruction of wing-tip vortex using vortex model, generation of BTVC using bubble dynamics model and acoustic wave prediction using the acoustic analogy. Because the CFD prediction of tip vortex structure generally suffers from severe under-prediction of its strength along the steamwise direction due to the intrinsic numerical damping of CFD schemes and excessive turbulence intensity, the wing-tip vortex along the freestream direction is regenerated by using the vortex modeling. Then, the bubble dynamics model based on the Rayleigh-Plesset equation was employed to simulate the generation and variation of BTVC. Finally, the flow noise due to BTVC is predicted by modeling each of spherical bubbles as a monople source whose strength is proportional to the rate of time-variation of bubble volume. The validity of the proposed numerical methods is confirmed by comparing the predicted results with the measured data.

CFD Analysis for Simulating Very-High-Temperature Reactor by Designing Experimental Loop (초고온가스로 모사 실험회로 설계를 위한 전산유체역학 해석)

  • Yoon, Churl;Hong, Sung-Deok;Noh, Jae-Man;Kim, Yong-Wan;Chang, Jong-Hwa
    • Transactions of the Korean Society of Mechanical Engineers B
    • /
    • v.34 no.5
    • /
    • pp.553-561
    • /
    • 2010
  • A medium-scale helium loop that can simulate a VHTR (very-high-temperature reactor) is now under construction at the Korea Atomic Energy Research Institute. The heaters of the test helium loop electrically heat helium fluid up to $950^{\circ}C$ at pressures of 1 to 9 MPa. To optimize the design specifications of the experimental helium loop, the conjugate heat transfer in the high-temperature helium heater was analyzed by performing a CFD simulation. The analysis results indicate that the maximum temperature does not exceed the allowable limit. It is confirmed that the thermal characteristics of the loop with the given geometry satisfy the design requirements.

Customized Aerodynamic Simulation Framework for Indoor HVAC Using Open-Source Libraries (공개 라이브러리 기반 실내 공조 맞춤형 전산모사 시스템 개발)

  • Sohn, Ilyoup;Roh, Hyunseok;Kim, Jaesung
    • Transactions of the Korean Society of Mechanical Engineers B
    • /
    • v.41 no.2
    • /
    • pp.135-143
    • /
    • 2017
  • A customized CFD simulator to perform thermo-fluid dynamic simulations of an HVAC for an indoor space is presented. This simulation system has been developed for engineers studying architectural engineering, as the HVAC mechanical systems used in housings and buildings. Hence, all functions and options are so designed to be suitable that they are suitable for non-CFD experts as well as CFD engineers. A Computational mesh is generated by open-source libraries, FEMM (Finite Element Method Magnetics), and OpenFOAM. Once the boundary conditions are set, the fluid dynamic calculations are performed using the OpenFOAM solver. Numerical results are validated by comparing them with the experimental data for a simple indoor air flow case. In this paper, an entirely new calculation process is introduced, and the flow simulation results for a sample office room are also discussed.

Effect of Air Flow Rate on the Performance of Planar Solid Oxide Fuel Cell using CFD (평판형 고체산화물 연료전지의 CFD 성능해석에서 공기유량변화의 영향)

  • Kim, Danbi;Han, Kyoungho;Yoon, Do-Young
    • Journal of the Korean Electrochemical Society
    • /
    • v.18 no.4
    • /
    • pp.172-181
    • /
    • 2015
  • Solid Oxide Fuel Cells (SOFC) continue to be among the most promising alternative energy devices. This paper addresses i-V characteristics of SOFC with a focus on air flow rate along the planar anode electrodes. To address this, detailed Butler-Volmer kinetics are implemented in a general-purpose CFD code FLUENT. The numerical results were validated against experimental data from the literature showing excellent match with i-V polarization data ranging 1V-0.4V. Numerical calculations of fuel cell operation under different flow rare conditions were performed in three-dimensional geometries. Results are presented in terms of concentration distribution of hydrogen, oxygen, and water. The simulations and results indicate that advanced CFD with UDF(User-Defined Function) of Butler-Volmer kinetics can be used to identify the conditions leading to air flow rate and specific surface area and guide development of operating conditions and improve the fuel cell system performance.

Design and Simulation of Fluidized Bed System for Waste Propellant Treatment by Computational Fluid Dynamics (폐 추진제 소각을 위한 유동층 반응기 설계 및 CFD 공정 모사)

  • Lee, Jiheon;Lee, Inkyu;Kim, Hyunsoo;Park, Jungsoo;Oh, Min;Moon, Il
    • Journal of the Korean Institute of Gas
    • /
    • v.22 no.2
    • /
    • pp.84-89
    • /
    • 2018
  • Recently, many studies have focused on the explosive waste treatment in terms of the safety and environmental pollution. A combustion process using fluidized bed incinerator has several profits : continuous process, low pollutive gases such as NOx, and high process efficiency. This study focused on the design of the propellant combustion reactor by using computational fluid dynamics(CFD) simulation technique. As a result, the reactions are successfully simulated in cylindrical incinerator, and. The study will influence to the research about treatment of explosive wastes.

Internal Flow Characteristics of Simulated Dual Pulse Rocket Motor by Using the Hot Gas and Cold Gas (Hot Gas와 Cold Gas를 이용한 모사 이중펄스 로켓 추진기관의 내부 유동 특성)

  • Cho, Kihong;Park, Jungho;Kim, Euiyong
    • Journal of the Korean Society of Propulsion Engineers
    • /
    • v.19 no.2
    • /
    • pp.1-8
    • /
    • 2015
  • Dual pulse rocket motor is a variant of solid rocket motor with two propellant grain separated by a pulse separation device. The major performance of such a rocket motor is influenced by the change in the hole area of pulse separation device to nozzle throat area ratio. In this study, we performed flow analysis to investigate the internal flow characteristics according to the pulse separation device hole area to nozzle throat area ratio change. Gases used flow analysis were used combustion gas of HTPB/AP composite propellant and nitrogen gas. Flow analysis results of the dual pulse rocket motor were validated by comparison with experimental results of pneumatics. Commercial CFD code ANSYS FLUENT 14.5 is used in this study to simulate flow analysis.