• Title/Summary/Keyword: 공기압력모델

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A Study on Alternative Fan Selection and Verification in Military Electronic Equipment (방산용 전자장비의 팬 선정 및 검증에 관한 연구)

  • Jin, Sung Eun;Kim, Hwan Gu;Yoon, Eui Youl;Jeon, Hee Ho;Kim, Seung Jun
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.41 no.11
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    • pp.1091-1097
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    • 2017
  • Sales of commercial-type cooling fans intended for application in military electronics are often discontinued during equipment production. This results in requirements for alternative fan selection as well as equipment performance and reliability tests, such as high-temperature operation testing. This study deals with alternative fan selection and verification methods that can be used during the production process. First, an alternative fan was selected by calculating the flow and pressure required to effectively cool the equipment, then the feasibility of the selected fan was verified using a reliable CFD heat dissipation analysis model. Following this, a high-temperature operation test was performed using the alternative fan in the equipment. Results demonstrated that the equipment satisfied its required function in a high-temperature environment, and the main parts as well as internal air temperature were found to be thermally stable.

An Experimental Study on Convection Heat Transfer in an Oscillating Flow of a Heater Tube for Stirling Cycle Machines (스터링 사이클기기용 가열기 원관내부 왕복유동에서의 열전달에 관한 실험적 연구)

  • 강병하;이건태;이춘식;이재헌
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.17 no.6
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    • pp.1547-1555
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    • 1993
  • An experimental study on convection heat transfer characteristics from a heated tube to an oscillating flow has been carried out, . This problem is of particular interest in the design of heat exchangers in Stirling cycle machines. Experimental system has been developed to measure temporal variations of temperature inside a heater tube during oscillating modes in a Stirling cycle machine. The dependence of temperature distributions and heat transfer rates on the oscillating frequency as well as the swept volume ratio and the mean pressure of a Stirling cycle machine is investigated in detail. The experimental results indicate that the measured temporal variations of temperature become nearly sinusoidal. The amplitude of temperature variation in the core of the tube is much more substantial than that near the tube wall, whereas the reverse is true for pulsating flows. It is also found that the heat transfer rate is increased significantly as the oscillating frequency or oscillating amplitude or the mean pressure in a tube is increased.

Combustion Test for a Supersonic Combustor Using a Direct-Connected Facility (직결형 설비를 이용한 초음속 연소기 연소 시험)

  • Yang, Inyoung;Lee, Kyung-Jae;Lee, Yang-Ji;Lee, Sanghoon;Kim, Hyungmo;Park, Poomin
    • Journal of the Korean Society of Propulsion Engineers
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    • v.22 no.3
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    • pp.1-7
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    • 2018
  • A combustion test for a supersonic combustor was conducted using a direct-connected type supersonic combustor test facility. The facility was verified for the capability of simulating required flow conditions. The test condition was maintained at Mach 2.0, $915^{\circ}C$ and 496 kPa for 15 s. Using gaseous hydrogen as the fuel, the combustor model was also tested for its ignition and flame holding capability at the fuel equivalence ratio of 0.12. Combustion efficiency was 71%, and the supersonic flow regime was obtained at this test condition.

An Experimental Study on Factors Affecting the Leachability of Cs-137 in Cement Matrix and Leaching Model with Backfill (시멘트 고화체내 Cs-137의 침출능에 영향을 미치는 인자에 대한 실험적 연구와 뒷채움재를 고려한 침출 모델)

  • Park, Jong-Kil;Lee, Kun-Jai
    • Nuclear Engineering and Technology
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    • v.23 no.4
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    • pp.374-386
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    • 1991
  • Various factors affecting the teachability of Cs-137 in cement matrix have been investigated. Factors investigated include such as pressure curing, vibration curing, pressure leaching, the effect of the clay addition, ion-exchange resin(IRN-77) addition, and $CO_2$or air injection. Leaching experiments were conducted by the method recommended by IAEA. To analyze the experimental results, pore structure analysis of cement matrices was carried out by BET method. Cement matrices may not contact directly with underground water in real repository, since the surroundings of disposed drums are filled with backfill. Thus, the effect of backfill to the teachability has been investigated. The well-known diffusion theory was utilized to predict long term leach rate and cumulative fraction leached of Cs-137 or non-radioactive species.

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Flow Characteristic of Cyclone Dust Separator for Marine Sweeping Machine (연마장비용 사이클론 집진기의 유동해석)

  • Park, MinJae;Jin, Taeseok
    • Journal of the Korean Institute of Intelligent Systems
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    • v.24 no.5
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    • pp.512-517
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    • 2014
  • This paper describes the development of new sweeping machine based on Cyclone Technology, which maintains constant suction power and uses it in a industrial applications as a method for dust removed from grinding work. The performance of a cyclone separator is determined by the turbulence characteristics and particle-particle interaction. To achieve this goal, we design cyclone technology based dust separator for sweeping machine has been proposed as a system which is suitable to work utilizing dust suction alternative to conventional manual system. and Numerical analysis with computational fluid dynamics(CFD) was carried out to investigate the working fluid that flow into cyclone dust separator in order to design optimal structure of the sweeping machine. The validation of cyclone model with CFD is carried out by comparing with experimental results.

Performance Analysis of Secondary Gas Injection for a Conical Rocket Nozzle TVC(II) (2차 가스분사에 의한 원추형 로켓노즐 추력벡터제어 성능해석 (II))

  • Song, Bong-Ha;Ko, Hyun;Yoon, Woong-Sup;Lee, Sang-Kil
    • Journal of the Korean Society of Propulsion Engineers
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    • v.5 no.1
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    • pp.18-25
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    • 2001
  • The results of systematic numerical experiments of secondary gas injection thrust vector control are presented. The effects of secondary injection system such as injection location and nozzle divergent cone angle onto the overall performance parameters such as thrust ratio, specific impulse ratio and axial thrust augmentation, are investigated. Complex nozzle exhaust flows induced by the secondary jet penetration is numerically analyzed by solving unsteady three-dimensional Reynolds-averaged Navier-Stokes equations with Baldwin-Lomax turbulence model for closure. Numerical simulations compared with the experiments of secondary air injection into the rocket nozzle of $9.6^{\cire}$ divergent half angle showed good agreement. The results obtained in terms of overall performance parameters showed that locating the secondary injection orifice further downstream of primary nozzle ensures the prevention of occurrence of reflected shock wave, therefore is suitable for efficient and stable thrust vectoring over a wide range of use.

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A Evaluation on the Field Application of High Strength Concrete for CFT Column (고강도 CFT용 콘크리트의 현장적용성 평가 및 장기거동 예측)

  • Park, Je Young;Chung, Kyung Soo;Kim, Woo Jae;Lee, Jong In;Kim, Yong Min
    • Journal of the Korea Concrete Institute
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    • v.26 no.6
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    • pp.707-714
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    • 2014
  • CFT (Concrete-Filled Tube) is a type of steel column comprised of steel tube and concrete. Steel tube holds concrete and the concrete inside tube takes charge of compressive load. This study presents structural performance of the CFT column which has 73~100 MPa high strength concrete inside. Fluidity, mechanical compression, pump pressure test in flexible pipe were conducted for understanding properties of the high strength concrete. Material properties were achieved by various experimental tests, such as slump, slump flow, air content, U-box, O-Lot, L-flow. In addition, mock-up tests were conducted to monitor concrete filling, hydration heat, compressive strength. From construction sites in Sang-am dong and University of Seo-kang, long-term behaviors could be effectively predicted in terms of ACI 209 material model considering elastic deformation, shrinkage and creep.

Performance analysis of a cold-air forced circulation type showcase (냉기 강제순환형 공랭식 쇼케이스 성능 해석)

  • Kim, Jeong-Sik;Kim, Nae-Hyun
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.14 no.3
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    • pp.1003-1010
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    • 2013
  • In this study, a simulation program was developed, which predicts the performance of cold-air forced circulation type air cooled showcase. The showcase has an excellent display effect in addition to preserving the grocery. In the program, the compressor was analyzed using performance data supplied by the manufacturer and the capillary tube pressure drop was analyzed using a homogeneous model. The evaporator and condenser were analyzed by dividing the heat exchangers into small elements, where energy balance and appropriate heat transfer correlations were used. A showcase model with two 3/4 HP compressors, capillary tubes of 1.6 mm inner diameter, a fin-and-tube evaporator and condenser was tested, and the results are compared with the predicted values. It is shown that both evaporation and condensation temperatures are adequately predicted by the program.

A Study on the Heat Flow Analysis of Infra-Red Signature Suppression System for Naval Ship (함정 적외선 신호저감 장치의 열 유동해석 연구)

  • Yoon, Seok-Tae;Cho, Yong-Jin;Ko, Dae-Eun
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.18 no.11
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    • pp.740-746
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    • 2017
  • Infrared signatures emitted from hot exhaust gases generated by the internal combustion engine and generator of naval ships and from the metal surfaces of the funnel have become the targets of infrared homing missiles, which is the main cause of a reduced survivability of naval ships. The infrared signatures from the exhaust gas and the metal surface of a funnel can be reduced by installing an infrared signature suppression (IRSS) system on a ship. The IRSS system consists of three parts: an eductor that generates turbulent flow of the exhaust gas, a mixing tube that mixes the exhaust gas with ambient air, and a diffuser that forms an air film using the pressure difference between the inside and outside air. As a basic study to develop an IRSS system using domestic technology, this study analyzed the model test conditions of an IRSS system developed by an overseas engineering company and installed on a domestic naval ship, and a numerical heat-flow analysis was conducted based on the results of the aforementioned analysis. Numerical heat-flow analysis was performed using a commercial numerical-analysis application, and various turbulence models were considered. As a result, the temperature and velocity of the exhaust gas at the educator inlet and diffuser outlet and that of the metal surface of the diffuser were measured, and found to agree well with the measurement results of the model test.

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.