• 제목/요약/키워드: heat generation mechanism

검색결과 82건 처리시간 0.025초

플라스틱성형용 KP-4M강의 마멸특성 및 이의 기구에 관한 연구 (A Study on the Wear Characteristics and the Mechanism of KP-4M Steel for Plastic Molding)

  • 박흥식;전태옥;김동호
    • Tribology and Lubricants
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    • 제12권1호
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    • pp.22-28
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    • 1996
  • This study was undertaken to investigate the dry wear characteristics and mechanism of KP-4M steel for plastic molding against SKD 61 hardened by heat treatment. The wear test was carried out under different conditions such as sliding speed, contact pressure, sliding distance, with frictional tester of pin on disc type. The wear loss on variation of sliding speed was little in lower speed range below 0.5 m/sec and in higher speed range above 1.5 m/sec,'but wear loss was high in intermediate speed range. The critical sliding speed, which showed the maximum value of specific wear rate, became lower with increased contact pressure. Increasing the contact pressure, the critical sliding distance Lcr which the wear mechanism changes from severe wear to mild wear was increased due to the decrease of oxidation reaction velocity. Through this study we suggested a model of generation and elimination process of wear debris of KP-4M steel for plastic molding.

하수처리시스템 온실가스 저감활동에 대한 CDM 사업 적용에 관한 연구 (An Application of CDM Project for Greenhouse Gas Reduction Activities in the Wastewater Treatment Systems)

  • 곽인호;황용우;조현정;박광호
    • 상하수도학회지
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    • 제24권3호
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    • pp.319-332
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    • 2010
  • In general, wastewater treatment systems consume high-energy consumption depending on operation characteristics of the facilities. Therefore, greenhouse gas(GHG) reduction activities that are application of digestion gas, induction of renewable energy etc. are conducted to reduce energy consumption and to increase energy independence ratio. In this study, GHG reduction in wastewater treatment system identified, searched application of Clean Development mechanism(CDM) approved methodology. If the methodologies apply to GHG reduction activities such as application of digestion gas, heat pump system using the wastewater as heat source, hydropower using the methodology determined CDM applicability, otherwise through several assumptions calculated expectable GHG reduction emissions and determined CDM applicability. As a result, the order of calculated GHG reduction emission showed that collected and energy generation of digestion gas is 66,775 $tCO_2$/yr, gas engine cogeneration system is 8,182 $tCO_2$/yr, heat pump system using the wastewater as a heat source is 72,715 $tCO_2$/yr, and hydropower is 561 $tCO_2$/yr. Consequently, the order of calculated Certified Emission Reductions(CERs) benefit showed that heat pump system using the wastewater, as a heat source is 1,381 million won/yr was estimated as the highest, followed by a collected and energy generation of digestion gas is 1,268 million won/yr.

THE COLLISION EFFECTS OF THE PARTICLES IN THE ACCRETION DISK

  • Yoo, K.H.
    • 천문학논총
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    • 제11권1호
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    • pp.125-137
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    • 1996
  • The collision of two particles in the accretion disk may lead to be a mechanism of heat generation. By using hydrodynamic equations, the mean free path, the collision frequency and the deflection angle due to the collision of the particles are derived as a function of the mass accretion rate. The mean free path seems to be a smaller fraction compared to the dimension parameter of the system. The radiative flux in the disk is obtained under the influence of the collision of the particles.

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압축성 유체의 급속 가열에 기인한 압력파의 생성 및 전달특성에 관한 연구 (A Study on the Generation and Transmission of a Pressure Wave Induced by Rapid Heating of Compressible Fluid)

  • 황인주;김윤제
    • 에너지공학
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    • 제12권1호
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    • pp.29-34
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    • 2003
  • 압력파의 일종인 열음향파는 압축성유체를 급속히 가열 또는 냉각하는 경계면 근처에서 유체가 순간적으로 압축 및 팽창하는 경우에 발생하는 현상으로 자연대류가 일어나지 않는 우주공간에서는 매우 중요한 열전달 메커니즘이다. 본 연구에서는 공기로 채워진 공간에서 급속한 가열에 의하여 발생한 열음향파의 전달특성을 수치적인 방법에 의하여 평가하고자 유한체적법을 기반으로 비정상 지배방정식을 이산화하였으며, PISO알고리즘과 2계 상향기법을 적용하여 해석을 수행하였다. 안정적인 수치해는 50 $\times$ 800 개의 셀과 1 $\times$ $10^{-9}$ 시간간격을 적용하여 얻을 수 있었으며, 생성된 열음향파는 유체 속을 통과하면서 점성과 열소산에 의하여 점점 감쇠하여 가는 경향을 보였다. 생성된 압력파는 날카로운 전단과 점점 감소하여 길게 늘어지는 후단부를 갖는 형상을 보였다.

페룰 가공용 초정밀 무심 연삭기의 열 특성 해석 (Thermal Characteristic Analysis of a High-Precision Centerless Grinding Machine for Machining Ferrules)

  • 김석일;조재완
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2005년도 춘계학술대회 논문집
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    • pp.90-95
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    • 2005
  • To perform the finish outside-diameter grinding process of ferrules which are widely used as fiber optic connectors, a high-precision centerless grinding machine is necessary. In this study, the thermal characteristics of the high-precision centerless grinding machine such as the temperature distribution, temperature rise and thermal deformation, are estimated based on the virtual prototype of the grinding machine and the heat generation rates of heat sources related to the machine operation conditions. The reliability of the predicted results is demonstrated by the temperature characteristics measured from the physical prototype. Especially, the predicted and measured results show the fact that the high-precision centerless grinding machine consisted of the hydrostatic GW and RW spindle systems, hydrostatic RW feeding mechanism, RW swivel mechanism, on-machine GW and RW dressers, and concrete-filled steel bed, has very stable thermal characteristics.

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의료용 초음파 위상배열 트랜스듀서의 열 분산 방안 (Thermal Dispersion Method for a Medical Ultrasonic Phased Array Transducer)

  • 이원석;노용래
    • 한국음향학회지
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    • 제34권3호
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    • pp.210-218
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    • 2015
  • 초음파 영상 품질의 향상을 위해 트랜스듀서의 구동전압을 높이게 되면 트랜스듀서에서 열이 발생하여 환자의 피부 화상 및 트랜스듀서의 성능 저하를 초래할 수 있다. 따라서, 이렇게 온도가 상승하지 않도록 트랜스듀서 내의 열을 효율적으로 분산할 수 있는 방안에 대해 연구하였다. 이때 열 분산 해석 대상으로 중심주파수가 3 MHz이고 32채널을 가진 위상배열 트랜스듀서를 선정하였다. 먼저 트랜스듀서의 동작에 따른 발열 구조를 이론적으로 분석하였고, 그 결과로서 재료의 감쇠와 음압의 크기가 발열에 영향을 미치는 것을 확인하였다. 나아가 유한요소 해석을 통해 트랜스듀서 구성소자의 물성이 열 분산에 미치는 영향을 분석하였다. 분석된 결과를 바탕으로 트랜스듀서 내 열이 잘 분산되기 위한 구성소자의 열물성을 정하였다. 도출된 열 물성을 유한요소 해석 모델에 적용한 결과 환자와 접촉되는 부분인 음향렌즈의 최고온도가 원래 값의 51 %로 저하되었다.

Computational Study on Unsteady Mechanism of Spinning Detonations

  • Matsuo, Akiko;Sugiyama, Yuta
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년도 학술대회
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    • pp.367-373
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    • 2008
  • Spinning detonations propagating in a circular tube were numerically investigated with a one-step irreversible reaction model governed by Arrhenius kinetics. Activation energy is used as parameter as 10, 20, 27 and 35, and the specific heat ratio and the heat release are fixed as 1.2 and 50. The time evolution of the simulation results was utilized to reveal the propagation mechanism of single-headed spinning detonation. The track angle of soot record on the tube wall was numerically reproduced with various levels of activation energy, and the simulated unique angle was the same as that of the previous reports. The maximum pressure histories of the shock front on the tube wall showed stable pitch at Ea=10, periodical unstable pitch at Ea=20 and 27 and unstable pitch consisting of stable, periodical unstable and weak modes at Ea=35, respectively. In the weak mode, there is no Mach leg on the shock front, where the pressure level is much lower than the other modes. The shock front shapes and the pressure profiles on the tube wall clarified the mechanisms of these stable and unstable modes. In the stable pitch at Ea=10, the maximum pressure history on the tube wall remained nearly constant, and the steady single Mach leg on the shock front rotated at a constant speed. The high and low frequency pressure oscillations appeared in the periodical unstable pitch at Ea=20 and 27 of the maximum pressure history. The high frequency was one cycle of a self-induced oscillation by generation and decay in complex Mach interaction due to the variation in intensity of the transverse wave behind the shock front. Eventually, sequential high frequency oscillations formed the low frequency behavior because the frequency behavior was not always the same for each cycle. In unstable pitch at Ea=35, there are stable, periodical unstable and weak modes in one cycle of the low frequency oscillation in the maximum pressure history, and the pressure amplitude of low frequency was much larger than the others. The pressure peak appeared after weak mode, and the stable, periodical unstable and weak modes were sequentially observed with pressure decay. A series of simulations of spinning detonations clarified that the unsteady mechanism behind the shock front depending on the activation energy.

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Computational Study on Unsteady Mechanism of Spinning Detonations

  • Matsuo, Akiko;Sugiyama, Yuta
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년 추계학술대회논문집
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    • pp.367-373
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    • 2008
  • Spinning detonations propagating in a circular tube were numerically investigated with a one-step irreversible reaction model governed by Arrhenius kinetics. Activation energy is used as parameter as 10, 20, 27 and 35, and the specific heat ratio and the heat release are fixed as 1.2 and 50. The time evolution of the simulation results was utilized to reveal the propagation mechanism of single-headed spinning detonation. The track angle of soot record on the tube wall was numerically reproduced with various levels of activation energy, and the simulated unique angle was the same as that of the previous reports. The maximum pressure histories of the shock front on the tube wall showed stable pitch at Ea=10, periodical unstable pitch at Ea=20 and 27 and unstable pitch consisting of stable, periodical unstable and weak modes at Ea=35, respectively. In the weak mode, there is no Mach leg on the shock front, where the pressure level is much lower than the other modes. The shock front shapes and the pressure profiles on the tube wall clarified the mechanisms of these stable and unstable modes. In the stable pitch at Ea=10, the maximum pressure history on the tube wall remained nearly constant, and the steady single Mach leg on the shock front rotated at a constant speed. The high and low frequency pressure oscillations appeared in the periodical unstable pitch at Ea=20 and 27 of the maximum pressure history. The high frequency was one cycle of a self-induced oscillation by generation and decay in complex Mach interaction due to the variation in intensity of the transverse wave behind the shock front. Eventually, sequential high frequency oscillations formed the low frequency behavior because the frequency behavior was not always the same for each cycle. In unstable pitch at Ea=35, there are stable, periodical unstable and weak modes in one cycle of the low frequency oscillation in the maximum pressure history, and the pressure amplitude of low frequency was much larger than the others. The pressure peak appeared after weak mode, and the stable, periodical unstable and weak modes were sequentially observed with pressure decay. A series of simulations of spinning detonations clarified that the unsteady mechanism behind the shock front depending on the activation energy.

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Development of a Mechanistic Model for Hydrogen Generation in Fuel-Coolant Interactions

  • Lee, Byung-Chul;Park, Goon-Cherl;Chung, Chang-Hyun
    • Nuclear Engineering and Technology
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    • 제29권2호
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    • pp.99-109
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    • 1997
  • A dynamic model for hydrogen generation by Fuel-Coolant Interactions(FCI) is developed with separate models for each FCI stage, coarse mixing and stratification. The model includes the physical concept of FCI, semi-empirical heat and mass transfer correlation and the concentration diffusion equation with the general non-zero boundary condition. The calculated amount of hydrogen, which is mainly generated in stratification, is compared with the FITS experiments. The model developed in this study shows a good agreement within a range of 10 % fuel oxidation rate and predicts the controlled mechanism of the chemical reaction very well. And this model predicts more accurately than the previous works. It is shown from the sensitivity study that the higher initial temperature of fuel particle is, the larger the reaction rate is. Up to 2700 K of temperature of the particle, the reaction rate increases rapid, which can lead to metal ignition.

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평판-휜 열교환기의 열-수력학적 성능에 대한 고속 바이패스 영향의 수치적 연구 (NUMERICAL STUDY OF THE HIGH-SPEED BYPASS EFFECT ON THE AERO-THERMAL PERFORMANCE OF A PLATE-FIN TYPE HEAT EXCHANGER)

  • 이준석;김민성;하만영;민준기
    • 한국전산유체공학회지
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    • 제22권1호
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    • pp.67-80
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    • 2017
  • The high-speed bypass effect on the heat exchanger performance has been investigated numerically. The plate-fin type heat exchanger was modeled using two-dimensional porous approximation for the fin region. Governing equations of mass, momentum, and energy equations for compressible turbulent flow were solved using ideal-gas assumption for the air flow. Various bypass-channel height were considered for Mach numbers ranging 0.25-0.65. Due to the existence of the fin in the bypass channel, the main flow tends to turn into the core region of the channel, which results in the distorted velocity profile downstream of the fin region. The boundary layer thickness, displacement thickness, and the momentum thickness showed the variation of mass flow through the fin region. The mass flow variation along the fin region was also shown for various bypass heights and Mach numbers. The volumetric entropy generation was used to assess the loss mechanism inside the bypass duct and the fin region. Finally, the correlations of the friction factor and the Colburn j-factor are summarized.