• Title/Summary/Keyword: 정압모델

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Combustion Test of a Mach 5 Scramjet Engine Model (마하 5 스크램젯 엔진 모델의 연소 시험)

  • Yang, Inyoung;Lee, Yang-Ji;Kim, Young-Moon;Lee, Kyung-Jae
    • Journal of the Korean Society of Propulsion Engineers
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    • v.17 no.3
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    • pp.9-14
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    • 2013
  • Combustion tests were conducted for a hydrogen-fueled Mach 5 scramjet engine model using a blow-down facility. No fuel and two fuel flow rate cases were tested for two different model configurations. Time history of the wall static pressures inside the model and their time-averaged spatial distribution were used for the analysis of the flow and combustion characteristics. For shorter model, supersonic combustion was occurred for both of the fuel flow rate cases. For longer model, supersonic combustion was occurred for less fuel case, whereas thermal choking and subsonic combustion were occurred for more fuel case. Intake started even for this subsonic combustion case.

Numerical Investigation about the Ground Test Results of Model Scramjet Engine (모델 스크램제트 엔진의 지상시험결과에 대한 전산해석연구)

  • Kang, Sang-Hun;Lee, Yang-Ji;Yang, Soo-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2008.05a
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    • pp.328-331
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    • 2008
  • In order to see the detailed characteristics of model scramjet engine, numerical analysis was performed and compared to the ground test results done by KARI and UQ. Pressure distribution predicted by numerical analysis showed good agreements with test results. Static temperature and pressure distribution explained the mechanisms of cavity flame holder and W-shape cowl which have showed enhancing effects on the supersonic combustion.

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Specific Heat Characteristics of Ceramic Fuels (산화물핵연료의 비열특성)

  • Kang Kweon Ho;Park Chang Je;Ryu Ho Jin;Song Kee Chan;Yang Myung Seung;Moon Heung Soo;Lee Young Woo;Na Sang Ho
    • Journal of Energy Engineering
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    • v.13 no.4
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    • pp.259-266
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    • 2004
  • Specific heat mechanism of oxide fuel is contributed by lattice vibration, dilatation, conduction electron and defect and excess specific heat. Model of oxide fuel for specific heat consists of specific heat at constant pressure term, dilatation specific heat term and defect specific heat term. In this study experimental and published data on the specific heats of oxide nuclear fuels have been reviewed and analyzed to recommend the best fitting model. The oxide fuels considered in this paper were UO$_2$, mixed (U, Pu) oxides and spent fuel. The specific heat data of spent fuel has been replaced by that of simulated fuel.

Isobaric Vapor-Liquid Equilibrium of Toluene and Cresol Systems (톨루엔-크레졸의 정압 기-액 평형)

  • Kang, Dong-Yuk;Jang, Hoi-Gu;Han, Chang-Nam;Rho, Seon-Gyun;Cho, Dong Lyun;Kang, Choon-Hyoung
    • Korean Chemical Engineering Research
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    • v.47 no.6
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    • pp.755-761
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    • 2009
  • To a first approximation, phase behavior of a system becomes increasingly skew in proportion to the boiling point difference of system-forming constituents. Therefore, phase behavior data of a system of a large boiling point difference are to be experimentally measured for thorough understanding of the thermodynamic characteristics of such system. In this work, isobaric vapor-liquid equilibrium of a mixture consisting of toluene and cresol, which shows a large boiling point difference of nearly $100^{\circ}C$ and is consequently expected to be considerably nonideal, was measured by using a recirculating equilibrium cell at various subatmospheric pressures ranging from 10 kPa to 60 kPa. The measured VLE data were correlated with NRTL and UNIQUAC models in a satisfactory manner and the accompanying thermodynamic consistency test represented soundness of the measurements. In addition, the excess molar volume of the mixture was also measured with a vibrating densitometer and correlated with a Redlich-Kister polynomial. A negative excess volume prevailed over the whole concentration range, which indicates a favorable attraction between toluene and cresol isomers and results in an extensive miscibility.

A Study of Interactive Training Methods for the Safe Operation of City Gas Governor (도시가스 정압기 안전운영을 위한 인터랙티브 훈련 방안 연구)

  • Kim, Hyoung Jean;Park, Chan Cook;Lee, Jae Yong;Lee, Chun Sik;Yu, Chul Hee
    • Journal of the Korean Institute of Gas
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    • v.21 no.1
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    • pp.34-42
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    • 2017
  • We developed the safety training methods which improve the current methods by overcoming the single scenario-based one-way communication between trainee and training system. We improved the design and implementation of the safety training scenarios, which is one of the most important components of the plant safety training system for safe operation of the city gas governor. The diversity and training effects of the training scenarios can be improved by interactive training between the plant safety training system and operators. The interactive training methods were developed based on Finite State Machine model which is applicable to and based on plant safety training platform. We could see the possibility of applying this method of safety training scenario system to other domain of plant safety training system.

Flow Dimensional Analysis for Constant Pressure Injection Test (정압주입시험을 이용한 지하수유동차원 해석)

  • 이은용
    • The Journal of Engineering Geology
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    • v.3 no.2
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    • pp.149-165
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    • 1993
  • Nowadays, the field hydraulic test is still an only method to evaluate groundwater characteristics in subsurface. The results of hydraulic test are very important for the concept model of fracture hydrogeology as well as the geometric pattern of fractures. The hydraulic tests performed in Korea are generally analysed under such assumption as steady radial flow in homogeneous aquifer or along simple geometry of fractures. Also the transmissivity measured in a fixed interval length is equivalent to a sum of individual fracture transmissivities in test legth. The boundary effects of weH hydraulics and the geometry of flow paths are hardly obtained from the test results analysed by a steady flow method. To circumvent this problem, the flow dimensional analysis was attempted from the results of constant pressure injection test carried out in a fractured granite area. A comparison of the hydraulic conductivity values from the transient and steady analysis shows that the latter is about a factor of 2~3 higher than the former. However, it was possible to analyse a flow dimension of each test interval from flow rate variation with time. The upper part of the bedrock(<10m deep) indicates an open boundary and the flow dimension shows nearly steady states, while the lower part of the bedrock(>25m deep) is characterized as sublinear flow dimension with a dosed boundary. In one of the test sections(15m deep), the flow dimension was changed from linear flow to spherical flow. From the experience of this study, one of the immediate problems to be solved is to enhance the field testing equipments, i.e., an accurate flowmeter with autorecording and a pressure detecting device to be able to install in the test section.

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Analysis of Turbulent Gas-Particle Suspension Flows in a Venturi (固體粒子 가 浮上된 벤츄리管 流動 의 解析)

  • 성형진;정명균
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.8 no.2
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    • pp.133-140
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    • 1984
  • A "two-fluid" equation model has been applied for predicting gas-solid suspension flows through a Venturi tube. In the "two-fluid"equation model, the bulk motion of the particles is considered as a continuum whose governing equation is obtained by averaging the conservation equations over a volume and expressing the equations in differential forms. Closure of the time-mean equations is achieved by modeling the turbulent correlations with an extended mixing-length theory. Proposed closure model is found to aptly simulate the dependency of the static pressure drop on the particle size, flow rate and the loading ratio.d the loading ratio.

An Experimental Study of Shock Wave Effects on the Model Scramjet Combustor (모델 스크램제트 연소기에서 충격파 영향에 대한 실험적 연구)

  • 허환일
    • Journal of the Korean Society of Propulsion Engineers
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    • v.3 no.1
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    • pp.65-71
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    • 1999
  • An experimental study was carried out in order to investigate the effect of shock waves on the supersonic hydrogen-air jet flames stabilized in the Mach 2.5 model scramjet combustor. This experiment was the first reacting flow experiment interacting with shock waves. Two identical $10^{\cire}$ wedges were mounted on the diverging sidewalls of the combustor in order to produce oblique shock waves that interacted with the flame. Schlieren visualization pictures, wall static pressures, and combustion efficiency at two different air stagnation temperatures were measured and compared to corresponding flames without shock wave-flame interaction. It was observed that shock waves significantly altered the shape of supersonic jet flames, but had different effects on combustion efficiency depending on air temperatures. At the higher air stagnation temperature and higher fuel flow rates, combustion of efficiency showed a better result.

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Analysis for Aerodynamic Resistance of Chrysanthemum Canopy through Wind Tunnel Test (풍동실험을 통한 국화군락의 공기유동 저항 분석)

  • Yu, In-Ho;Yun, Nam-Kyu;Cho, Myeong-Whan;Lee, In-Bok
    • Journal of Bio-Environment Control
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    • v.17 no.2
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    • pp.83-89
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    • 2008
  • A wind tunnel test was conducted at Protected Horticulture Experiment Station of National Horticultural Research Institute in Busan to find the aerodynamic resistance and quadratic resistance coefficient of chrysanthemum in greenhouse. The internal plants of the CFD model has been designed as a porous media because of the complexity of its physical shapes. Then the aerodynamic resistance value should be input for analyzing CFD model that crop is considered while the value varies by crops. In this study, the aerodynamic resistance value of chrysanthemum canopy was preliminarily found through wind tunnel test. The static pressure at windward increased as wind velocity and planting density increased. The static pressure at leeward decreased as wind velocity increased but was not significantly affected by planting density. The difference of static pressure between windward and leeward increased as wind velocity and planting density increased. The aerodynamic resistance value of chrysanthemum canopy was found to be 0.22 which will be used later as the input data of Fluent CFD model. When the planting distances were $9{\times}9\;cm$, $11{\times}11\;cm$, and $13{\times}13\;cm$, the quadratic resistance coefficients of porous media were found to be 2.22, 1.81, and 1.07, respectively. These values will be used later as the input data of CFX CFD model.

Numerical Analysis on the Stress Behaviours Due to Geometry Effects of the Membrane Corrugation (멤브레인의 주름 형상이 응력거동에 미치는 영향에 관한 수치적 해석)

  • Kim Chung-Kyun;Lee Young-Suck;Cha Baeg-Soon;Kim Young-Gyu;Yoon In Soo;Hong Seong Ho
    • Journal of the Korean Institute of Gas
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    • v.1 no.1
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    • pp.21-26
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    • 1997
  • This paper presents the numerical results of six corrugation models which compute the stress behaviours and stress levels of the membrane structure under the hydrostatic pressure of cryogenic liquids and thermal loadings using a non -linear finite element analysis program. A three-dimensional analysis of various corrugation geometries was performed on the maximum mean normal stress distributions along the upper surface of the membrane sheet. Comparisons of the FEM results for various geometry models of the corrugation are presented, which shows that the corrugated configuration of the ring knot model can be effectively performed for the combined forces such as the hydrostatic pressure and thermal loading in comparison with the Technigaz type corrugation which has small comer and apex curvatures. The FEM results show that the ring knot corrugation can be used for the deepest depth, 180m of the LNG storage tank in comparison with other corrugation models.

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