• Title/Summary/Keyword: 기체역학

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Thermodynamic Analysis of Re-liquefaction Cycle of LNG Boil-off Gas (LNG 증발기체의 재액화 사이클에 대한 열역학 해석)

  • Chin, Young-Wook;Moon, Jeong-Woo;Lee, Yoon-Pyo;Chang, Ho-Myung
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.19 no.7
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    • pp.485-490
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    • 2007
  • The LNG BOG re-liquefaction system for LNG carriers was designed based on the Claude refrigeration cycle and the thermodynamic analysis was carried out in order to find the design point of the three heat exchangers constituting the system. The thermodynamic analysis revealed that the system state could be defined by the three cold endpoint temperatures of the three-pass heat exchanger. Hence the iso-lines of the specific liquefaction work, taken as the performance indicator, were presented in terms of those three temperatures and discussed. The system was found most economical when those three temperatures approached a single temperature of $-140^{\circ}C$ and thus this system state could be taken as the design point for the heat exchangers.

Numerical study on PEM fuel cell performance with variation of GDL permeability and channel geometry (기체확산층의 유동투과율과 채널 형상 변화에 따른 고분자 전해질 연료전지 성능변화 수치연구)

  • Koh, Soo-Gon;Sohn, Sang-Ho;Nam, Jin-Hyun;Kim, Charn-Jung
    • Proceedings of the KSME Conference
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    • 2008.11b
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    • pp.3114-3119
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    • 2008
  • Relatively high convective flow exists in the under-rib regions of a gas diffusion layer (GDL) when serpentine flow fields are employed in a PEMFC. This under-rib convection is believed to be favorable for the performance of PEMFCs, by enabling more effective use of catalysts in the under-rib regions. From the fact that the under-rib convection in a GDL is directly proportional to the permeability of the GDL, computational fluid dynamics (CFD) simulations were performed to discover the relationship between the GDL permeability and the PEMFC performance. Single-, triple-, and quintuple-path parallel serpentine flow fields for $9\;cm^2$ active cell area were considered while changing the GDL permeability from $1{\times}10^{-12}$ to $5{\times}10^{-11}m^2$. The results showed that higher GDL permeability generally resulted in better performance of PEMFCs, but the degree of performance enhancement became smaller as the parallel path number increased. The effects of the permeability on the local variables were also discussed.

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Numerical Analysis on the Compressible Flow Characteristics of Supersonic Jet Caused by High-Pressure Pipe Rupture Using CFD (CFD를 이용한 고압파이프 파단 시 초음속제트의 압축성유동 특성에 관한 수치해석)

  • Jung, Jong-Kil;Kim, Kwang-Chu;Yoon, Jun-Kyu
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.41 no.10
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    • pp.649-657
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    • 2017
  • A rupture in a high-pressure pipe causes the fluid in the pipe to be discharged in the atmosphere at a high speed resulting in a supersonic jet that generates the compressible flow. This supersonic jet may display complicated and unsteady behavior in general. In this study, Computational Fluid Dynamics (CFD) analysis was performed to investigate the compressible flow generated by a supersonic jet ejected from a high-pressure pipe. A Shear Stress Transport (SST) turbulence model was selected to analyze the unsteady nature of the flow, which depends upon the various gases as well as the diameter of the pipe. In the CFD analysis, the basic boundary conditions were assumed to be as follows: pipe of diameter 10 cm, jet pressure ratio of 5, and an inlet gas temperature of 300 K. During the analysis, the behavior of the shockwave generated by a supersonic jet was observed and it was found that the blast wave was generated indirectly. The pressure wave characteristics of hydrogen gas, which possesses the smallest molecular mass, showed the shortest distance to the safety zone. There were no significant difference observed for nitrogen gas, air, and oxygen gas, which have similar molecular mass. In addition, an increase in the diameter of the pipe resulted in the ejected impact caused by the increased flow rate to become larger and the zone of jet influence to extend further.

An Experimental Study on the Spray Characteristics of a Rotating Fuel Nozzle of a Slinger Combustor for Different Flow Rates and Rotating Speeds (슬링거 연소기 회전연료노즐의 유량과 회전수에 따른 분무특성에 대한 실험적 연구)

  • Shim, Hyeon-Seok;Bae, Jonggeun;Kim, Jupyoung;Kim, Shaun;Kim, Donghyun;Ryu, Gyongwon
    • Journal of the Korean Society of Propulsion Engineers
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    • v.25 no.4
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    • pp.59-70
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    • 2021
  • An experimental study was conducted to observe the spray characteristics for different flow rates and rotating speeds of a rotating fuel nozzle of a slinger combustor. The water spray ejected from the nozzle orifice was visualized using a high-speed camera and a light source. It was confirmed that the atomization was improved, as the flow rate decreased and rotating speed increased. The characteristic maps for the spray characteristics and performance parameters showed that the aerodynamic Weber number and the liquid-air momentum flux ratio were associated with the liquid primary breakup, and the liquid-air momentum flux ratio and Rossby number were closely correlated with the liquid ejection mode.

A Numerical Study of Cathode Block and Air Flow Rate Effect on PEMFC Performance (고분자전해질 연료전지의 환원극 블록과 공기 유량 영향에 대한 전산 해석 연구)

  • Jo, Seonghun;Kim, Junbom
    • Applied Chemistry for Engineering
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    • v.33 no.1
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    • pp.96-102
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    • 2022
  • Reactants of PEMFC are hydrogen and oxygen in gas phases and fuel cell overpotential could be reduced when reactants are smoothly transported. Numerous studies to modify cathode flow field design have been conducted because oxygen mass transfer in high current density region is dominant voltage loss factor. Among those cathode flow field designs, a block in flow field is used to forced supply reactant gas to porous gas diffusion layer. In this study, the block was installed on a simple fuel cell model. Using computational fluid dynamics (CFD), effects of forced convection due to blocks on a polarization curve and local current density contour were studied when different air flow rates were supplied. The high current density could be achieved even with low air supply rate due to forced convection to a gas diffusion layer and also with multiple blocks in series compared to a single block due to an increase of forced convection effect.

Study on Thermophysical Property Characteristics of a 4 Species Kerosene Surrogate in a Swirl Injector at Supercritical Pressure Condition (초임계 압력 조건 스월 인젝터에서 4개 화학종 혼합물 케로신 대체 모델의 열역학 물성 특성 연구)

  • Kim, Kukjin;Heo, Junyoung;Sung, Honggye
    • Journal of the Korean Society of Propulsion Engineers
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    • v.17 no.6
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    • pp.48-58
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    • 2013
  • Characteristics of thermophysical properties and flow structures in a swirl injector at supercritical pressure have been investigated using the kerosene surrogate consisting of four species and various ideal and real gas equations of state. The quantitative comparisons of thermophysical properties for equations of state have been performed. Also, a large eddy simulation and preconditioning technique for getting an effective convergence rate are applied to analyze turbulent flow in a swirl injector. The flow characteristics in the injector has significantly different behaviors depending on the equations of state due to the different thermophysical properties in the injector. The Redlich-Kwong-Peng-Robinson equation of state provides the most suitable results in the wide range of temperature.

Vibration Reduction Simulation of UH-60A Helicopter Airframe Using Active Vibration Control System (능동 진동 제어 시스템을 이용한 UH-60A 헬리콥터 기체의 진동 감소 시뮬레이션)

  • Lee, Ye-Lin;Kim, Do-Young;Kim, Do-Hyung;Hong, Sung-Boo;Park, Jae-Sang
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.48 no.6
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    • pp.443-453
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    • 2020
  • This study using the active vibration control technique attempts to alleviate numerically the airframe vibration of a UH-60A helicopter. The AVCS(Active Vibration Control System) is applied to reduce the 4/rev vibration responses at the specified locations of the UH-60A airframe. The 4/rev hub vibratory loads of the UH-60A rotor is predicted using the nonlinear flexible dynamics analysis code, DYMORE II. Various tools such as NDARC, MSC.NASTRAN, and MATLAB Simulink are used for the AVCS simulation with five CRFGs and seven accelerometers. At a flight speed of 158knots, the predicted 4/rev hub vibratory loads of UH-60A rotor excite the airframe, and then the 4/rev vibration responses at the specified airframe positions such as the pilot seat, rotor-fuselage joint, mid-cabin, and aft-cabin are calculated without and with AVCS. The 4/rev vibration responses at all the locations and directions are reduced by from 25.14 to 96.05% when AVCS is used, as compared to the baseline results without AVCS.

Characteristics of Plasma Discharge according to the Gas-flow Rate in the Atmospheric Plasma Jets (대기압 플라즈마 제트의 기체 유량에 대한 방전 특성)

  • Lee, Won Young;Jin, Dong Jun;Kim, Yun Jung;Han, Gook Hee;Yu, Hong Keun;Kim, Hyun Chul;Jin, Se Whan;Koo, Je Huan;Kim, Do Young;Cho, Guangsup
    • Journal of the Korean Vacuum Society
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    • v.22 no.3
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    • pp.111-118
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    • 2013
  • The influence of gas flow on the plasma generation in the atmospheric plasma jet is described with the theory of hydrodynamics. The plasma discharge is affected by the gas-flow streams with Reynolds number (Re) as well as the gas pressure with Bernoulli's theorem according to the gas flow rate inserted into the glass tube. The length of plasma column is varied with the flow types such as the laminar flow of Re<2,000 and the turbulent flow of Re>4,000 as it has been known in a general fluid experiments. In the laminar flow, the plasma column length is increased as the increase of flow rate. Since the pressure in the glass tube becomes low as the increase of flow velocity by the Bernoulli's theorem, the breakdown voltage of plasma discharge is reduced by the Paschen's law. Therefore, the plasma length is increased as the increasing flow rate with the fixed operation voltage. In the transition of laminar and turbulent flows, the plasma length is decreased. When the flow becomes turbulent as the flow rate is increasing, the plasma length becomes short and the discharge is shut down ultimately. In the discharge of laminar flow, the diameter of plasma beam exposed on the substrate surface is kept less than the glass diameter, since the gas flow is kept to the distinct distance from the nozzle of glass tube.

The Comparison of Proton Exchange Membrane Fuel Cell According to Flow Field Design (고체고분자전해질형 연료전지의 유로형상에 따른 성능의 비교)

  • LEE, KEON JOO
    • Journal of Digital Convergence
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    • v.19 no.5
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    • pp.279-284
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    • 2021
  • In this study, the performance and distribution of fluid concentration, pressure, and current density of a proton exchange membrane fuel cell was investigated. In this paper, the two different types of flow field design were compared, singel channel and 5-channels. As a result, the 5-channels of flow field showed the better performance than that of single chanel. Especially, the single channel showed better performance in terms of mass transfer loss area.

Effects of Thermal Dispersion Damage on the Pyrolysis and Reactor Relarionship Using Comutational Fluids Dynamics (전산유체역학을 활용한 폐플라스틱열분해 반응기의 기체분산판에 대한 유동해석)

  • Jongil, Han;SungSoo, Park;InJea, Kim;Kwangho, Na
    • New & Renewable Energy
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    • v.19 no.4
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    • pp.53-60
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    • 2023
  • The Computational Fluid Dynamics (CFD) model is a method of studying the flow phenomenon of fluid using a computer and finding partial differential equations that dominate processes such as heat dispersion through numerical analysis. Through CFD, a lot of information about flow disorders such as speed, pressure, density, and concentration can be obtained, and it is used in various fields from energy and aircraft design to weather prediction and environmental modeling. The simulation used for fluid analysis in this study utilized Gexcon's (FLACS) CODE, such as Norway, through overseas journals, for the accuracy of the analysis results through many experiments. It was analyzed that a technology for treating two or more catalysts with physical properties under low-temperature atmospheric pressure conditions could not be found in the prior art. Therefore, it would be desirable to establish a continuous plan by reinforcing data that can prove the effectiveness of producing efficient synthetic oil (renewable oil) through the application that pyrolysis under low-temperature and atmospheric pressure conditions.