• 제목/요약/키워드: Thermal Equilibrium

검색결과 376건 처리시간 0.029초

유니베이커 오븐의 유동해석 (CFD Analysis of Unibaker Oven)

  • 이종선;백두성
    • 한국산학기술학회논문지
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    • 제5권5호
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    • pp.371-376
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    • 2004
  • 본 논문은 열평형 기술을 활용하여 다단계 조절이 가능한 유니베이커 오븐에 대하여 CFD(computational fluid dynamics) 해석을 수행하여 오븐내부의 열유동분포와 속도를 파악함으로서 오븐 내부의 열평형을 이룰 수 있는 최적 위치를 예상함으로서 유니베이커 오븐의 설계 자료로 이용하고자 한다.

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양생조건·외기온도·비등효과를 고려한 콘크리트 외기대류계수의 결정 (Determination of Convection Heat Transfer Coefficient Considering Curing Condition, Ambient Temperature and Boiling Effect)

  • 최명성;김윤용;우상균;김진근
    • 콘크리트학회논문집
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    • 제17권4호
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    • pp.551-558
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    • 2005
  • 이 연구에서는 외기와의 열전달을 나타내는 외기대류계수에 관한 실험을 실시하였다. 외기대류계수에 관한 기존의 모델에서 나타났던 문제점을 해결하기 위해 실험 변수로 풍속외에 양생 조건의 종류(양생포, 양생포+비닐), 외기온도, 비등효과를 선정하였다. 실험 결과를 이용하여 외기대류계수를 산정하고자 열평형 방정식을 이용한 수치해법을 사용하였으며, 이론적인 고찰을 통해 각 양생 조건별로 풍속에 따른 외기대류계수의 변화를 예측할 수 있는 모델식을 제안하였다. 열평형 방정식을 이용한 수치해법에서 초기에 외기대류계수가 과잉평가되는 문제점을 해결하기 위해 비등효과에 의한 증발량을 고려하여 수정 열평형 방정식을 제안하였다. 양생 조건을 고려한 제안된 모델식에 의하면, 모든 경우에 풍속에 따라 외기대류계수가 증가하는 경향을 보였으나 양생 재료의 사용여부나 양생 조건에 따라 다른 양상을 보이는 것을 알 수 있었다. 이러한 양상의 차이는 양생 재료의 열 특성에 의해 결정되는 것으로 외기대류계수는 양생 재료가 없는 경우, 양생포를 사용한 경우, 양생포+비닐을 사용한 경우의 순으로 풍속의 영향을 받는 것으로 나타났다. 제안된 모델식을 이용하면 수화열에 의한 콘크리트 구조물의 온도해석시 보다 정확한 결과를 얻을 수 있을 것으로 사료되며, 향후 이러한 열특성계수에 대한 연구가 필요할 것으로 판단된다.

열 질식에 의한 덕티드 로켓 가스 발생기의 연소 압력 상승 (A Sudden Increase in Combustion Pressure of Gas Generator of Ducted Rocket by Thermal Choking)

  • 김도영;신경훈;이창진
    • 한국항공우주학회지
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    • 제43권8호
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    • pp.684-691
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    • 2015
  • 덕티드 로켓 가스발생기용 추진제 성능을 검증하기 위한 실험에서 직경이 10mm인 파이프와 최소 직경이 8.7mm인 수축 노즐을 배출 튜브로 사용하였을 때 급격한 압력 증가가 관찰되었다. 급격한 연소 압력 증가는 배출 튜브를 통과하는 유동의 열 질식(thermal choking) 때문인 것으로 판단하였다. 본 연구에서는 원형 파이프를 사용하는 경우, 배출 튜브 유동의 열 질식을 고려하여 가스발생기 연소 압력 변화를 예측하였다. 그 결과, 배출가스의 비-평형 화학반응으로 인한 배출 튜브 유동의 열 질식 발생이 급격한 연소 압력 증가의 원인임을 확인하였다. 특히 덕티드 로켓의 높은 압력 지수는 배출 튜브 내에서 발생하는 열에 매우 민감하게 반응하여 배출 튜브 내의 열 질식 가능성을 높이는 것으로 분석되었다. 또한 배출 튜브로 단면적의 변화가 있는 발산형 파이프를 사용하면 가스발생기의 급격한 연소 압력 증가를 예방할 수 있을 것으로 판단하였다.

Bending analysis of an imperfect FGM plates under hygro-thermo-mechanical loading with analytical validation

  • Daouadji, Tahar Hassaine;Adim, Belkacem;Benferhat, Rabia
    • Advances in materials Research
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    • 제5권1호
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    • pp.35-53
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    • 2016
  • Flexural bending analysis of perfect and imperfect functionally graded materials plates under hygro-thermo-mechanical loading are investigated in this present paper. Due to technical problems during FGM fabrication, porosities and micro-voids can be created inside FGM samples which may lead to the reduction in density and strength of materials. In this investigation, the FGM plates are assumed to have even and uneven distributions of porosities over the plate cross-section. The modified rule of mixture is used to approximate material properties of the FGM plates including the porosity volume fraction. In order the elastic coefficients, thermal coefficient and moisture expansion coefficient of the plate are assumed to be graded in the thickness direction. The elastic foundation is modeled as two-parameter Pasternak foundation. The equilibrium equations are given and a number of examples are solved to illustrate bending response of Metal-Ceramic plates subjected to hygro-thermo-mechanical effects and resting on elastic foundations. The influences played by many parameters are investigated.

Horizontal Firing Boiler의 열유동 해석 (Numerical Analysis on Flow and Heat Transfer of Horizontal Firing Boiler)

  • 김광추;박만흥;김종길;최청렬;강대웅;김창녕
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 춘계학술대회논문집D
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    • pp.973-978
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    • 2001
  • Numerical Analysis for liquid fuel combustion of horizontal firing boiler is performed. The mixture-fraction/PDF equilibrium chemistry model is used to predict the combustion of the vaporized fuel. P1 model for radiation effect is used. Superheater, reheater and economizer is modeled using porous with heat sink. Flow and temperature field is investigated, and distribution of thermal $NO_{x}$ and CO is investigated. Computation as the change of excess air and swirling is performed to investigate the change of thermal $NO_{x}$.

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액체로켓의 재생냉각채널에 대한 열해석 프로그램의 개발 및 난류열유동 해석 (Development of a Thermal Analysis Program for a Regenerative Cooling Passage of Liquid Rocket and Simulation of Turbulent Heat Transfer)

  • 박태선
    • 한국전산유체공학회지
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    • 제8권3호
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    • pp.56-65
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    • 2003
  • A numerical procedure for analyzing the heat transfer in a regenerative cooling passage of liquid rocket has been developed. The thermal analysis is based on the numerical model of Naraghi〔1〕. The thermodynamic and transport properties of the combustion gases are evaluated using the chemical equilibrium composition. The pressure and heat flux obtained by the isentropic relation are in good agreement with the result of Navier-Stokes equations. The effect of design parameters on heat transfer is addressed for the pressure loss and temperature variation. Also, their constraints in designing the cooling passage are recommended. Finally, in a heated rectangular duct, the effects of secondary flow on heat transfer are scrutinized by the nonlinear k- e -fu of Park et at.〔2〕.

Air-Water 모델에서 기포특성에 관한 실험적 연구 (An Experimental Study on the Characteristics of Bubbles in Air-Water Model)

  • 오율권;서동표
    • 한국안전학회지
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    • 제18권1호
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    • pp.14-18
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    • 2003
  • The structural development of air-water bubble plumes has been measured under different condition on air flow rate in a cylindrical bath. The time-averaged structure of plumes has been measured with an oscilloscope and an electro-conductivity probe. The temperature of bubbles was also obtained by a thermal-infrared camera. Gas volume fraction and bubble frequency were high since bubbles concentrated on the nozzle. In general, their axial and radial values tended to decrease with increasing distance. Bubble temperature reached water temperature within a short time. The present study showed that thermal equilibrium between bubbles and water was completed before bubbles flow became stable.

인젝터 플라즈마 저항의 실험적 연구 (An experimental study on the resistivity of injector plasma)

  • 한충규
    • 한국군사과학기술학회지
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    • 제5권4호
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    • pp.19-26
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    • 2002
  • A chamber enduring 3,000 bars and an electrical high voltage power system have been designed and installed for studying the characteristics of the plasma produced in electro-thermal chemical propulsion system. In order to test the structural characteristics, polyethylene injectors were used which have 4 or 6 mm inner diameter and several lengths from 15 to 70 mm. The capacitors were charged at the voltages of 5.2, 7.3 and 10.4 kV which correspond to 5.58, 11 and 22.3 kJ in charging energy. The observed resistivities of the plasma injector are close to those predicted by a theoretical model that describes the plasma resistivity according to high current density.

Thermomechanical postbuckling of imperfect moderately thick plates on two-parameter elastic foundations

  • Shen, Hui-Shen
    • Structural Engineering and Mechanics
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    • 제4권2호
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    • pp.149-162
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    • 1996
  • A postbuckling analysis is presented for a simply supported, moderately thick rectangular plate subjected to combined axial compression and uniform temperature loading and resting on a two-parameter elastic foundation. The two cases of thermal postbuckling of initially compressed plates and of compressive postbuckling of initially heated plates are considered. The initial geometrical imperfection of the plate is taken into account. The formulations are based on the Reissner-Mindlin plate theory considering the first order shear deformation effect, and including the plate-foundation interaction and thermal effect. The analysis uses a deflection-type perturbation technique to determine the buckling loads and postbuckling equilibrium paths. Numerical examples cover the performances of perfect and imperfect, moderately thick plates resting on Winkler or Pasternak-type elastic foundations. Typical results are presented in dimensionless graphical form.

Arcjet Thruster 유동의 전산해석 (NUMERICAL FLOW FIELD ANALYSIS OF AN ARCJET THRUSTER)

  • 신재렬;최정열
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2006년도 추계 학술대회논문집
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    • pp.101-105
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    • 2006
  • The computational fluid dynamic analysis has been conducted for the thermo-chemical flow field in an arcjet thruster with mono-propellant Hydrazine (N2H4) as a working fluid. The Reynolds Averaged Navier-Stokes (RANS) equations are modified to analyze compressible flows with the thermal radiation and electric field. The Maxwell equation, which is loosely coupled with the fluid dynamic equations through the Ohm heating and Lorentz forces, is adopted to analyze the electric field induced by the electric arc. The chemical reactions of Hydrazine were assumed to be infinitely fast due to the high temperature field inside the arcjet thruster. The chemical and the thermal radiation models for the nitrogen-hydrogen mixture and optically thick media respectively, were incorporated with the fluid dynamic equations. The results show that performance indices of the arcjet thruster with 1kW arc heating are improved by amount of 180% in thrust and 200% in specific impulse more than frozen flow. In addition to thermo-physical process inside the arcjet thruster is understood from the flow field results.

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