• 제목/요약/키워드: Hot Wall Method

검색결과 228건 처리시간 0.028초

NUMERICAL ANALYSIS FOR PRANDTL NUMBER DEPENDENCY ON NATURAL CONVECTION IN AN ENCLOSURE HAVING A VERTICAL THERMAL GRADIENT WITH A SQUARE INSULATOR INSIDE

  • Lee, Jae-Ryong;Park, Il-Seouk
    • Nuclear Engineering and Technology
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    • 제44권3호
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    • pp.283-296
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    • 2012
  • The natural convection in a horizontal enclosure heated from the bottom wall, cooled at the top wall, and having a square adiabatic body in the center is studied. Three different Prandtl numbers (0.01, 0.7 and 7) are considered for the investigation of the effect of the Prandtl number on natural convection. Adiabatic boundary conditions are employed for the side walls. A two-dimensional solution for unsteady natural convection is obtained, using an accurate and efficient Chebyshev spectral methodology for different Rayleigh numbers varying over the range of $10_3$ to $10_6$. It had been experimentally reported that the heat transfer mode becomes oscillatory when Pr is out of a specific Pr band beyond the critical Ra. In this study, we reproduced this phenomenon numerically. It was found that when Ra=$10_6$, only the case for intermediate Pr (=0.7) reached a non-changing steady state and the low and high Pr number cases (Pr=0.01 and 7) showed a periodically oscillatory fashion hydrodynamically and thermally. The variation of time- and surface-averaged Nusselt numbers on the hot and cold walls for different Rayleigh numbers and Prandtl numbers are presented to show the overall heat transfer characteristics in the system. Further, the isotherms and streamline distributions are presented in detail to compare the physics related to their thermal behavior.

초음속충돌제트의 열전달에 관한 실험적 연구 (Experimental Study on the Heat Transfer of Supersonic Impinging Jet)

  • 이찬;정명균
    • 대한기계학회논문집
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    • 제15권1호
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    • pp.323-327
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    • 1991
  • 본 연구에서는 로켓노즐로 부터 분출되는 고온의 초음속제트가 45˚로 경사진 평판으로 분사되는 경우의 열전달을 측정하였다.고온의 제트가 충돌하는 평판표면 의 고온과 열유속을 측정하는 것이 거의 불가능하므로, 국소적열전달은 국소적 준 1차 원 열전도모형을 평판표면 아래에서 측정한 온도자료에 적용하여 구하였다.

나선형코일 튜브 비등2상 유동 수치해석 (Numerical Simulation of Boiling 2-Phase Flow in a Helically-Coiled Tube)

  • 조종철;김웅식;김효정;이용갑
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2004년도 춘계 학술대회논문집
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    • pp.49-55
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    • 2004
  • This paper addresses a numerical simulation of the flow and heat transfer in a simplified model of helically coiled tube steam generator using a general purpose computational fluid dynamic analysis computer code. The steam generator model is comprised of a cylindrical shell and helically coiled tubes. A cold feed water entered the tubes is heated up, evaporates. and finally become a superheated steam with a large amount of heat transferred continuously from the hot compressed water at higher pressure flowing counter-currently through the shell side. For the calculation of tube side two-phase flow field formed by boiling, inhomogeneous two-fluid model is used. Both the internal and external turbulent flows are simulated using the standard k-e model. The conjugate heat transfer analysis method is employed to calculate the conduction in the tube wall with finite thickness and the convections in the internal and external fluids simultaneously so as to match the fluid-wall-fluid interface conditions properly. The numerical calculations are peformed for helically coiled tubes of steam generator at an integral type pressurized water reactor under normal operation. The effects of tube-side inlet flow velocity are discussed in details. The results of present numerical simulation are considered to be physically plausible based on the data and knowledge from previous experimental and numerical studies where available.

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주기적 통과 후류의 방향과 주파수가 익형 위 비정상 천이경계층에 미치는 영향 (Effects of Wake-Passing Orientation and Frequency on Unsteady Boundary Layer Transition on an Airfoil)

  • 강신형;박태춘;전우평
    • 대한기계학회논문집B
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    • 제26권5호
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    • pp.685-694
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    • 2002
  • Effects of wake-passing orientation and frequency on the wake-induced boundary layer transition on a NACA0012 airfoil are investigated. The wakes are generated by rotating cylinders clockwise (CW) and counterclockwise (CCW) around the airfoil. Time- and phase-averaged streamwise mean velocities and turbulent fluctuations are measured with a single hot-wire probe. Wall skin frictions are estimated by the Computational Preston Tube Method (CPM). The pressure distribution on the airfoil is different according to the wake-passing orientation and frequency. Turbulent patches are generated in the laminar boundary layer due to the passing wake and the boundary layer becomes temporarily transitional. The transition process is significantly affected by the pressure gradient and the turbulent patches. For the receding wake, the turbulent patches propagate more rapidly than those for the approaching wake because adverse pressure gradient becomes larger. As the frequency increases, onset location of transition moles upstream and the boundary layer near the trailing edge becomes more transitional.

사각 단열체가 존재하는 밀폐계 내부에서 Pr수 변화에 따른 자연대류 현상에 대한 수치적 연구 (NUMERICAL STUDY FOR PRANDTL NUMBER DEPENDENCY ON NATURAL CONVECTION IN AN ENCLOSURE WITH SQUARE ADIABATIC BODY)

  • 이재룡
    • 한국전산유체공학회지
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    • 제16권3호
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    • pp.29-36
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    • 2011
  • The natural convection in a horizontal enclosure heated from the bottom wall, cooled at the top wall, and having a square adiabatic body at its centered area was studied. Three different Prandtl numbers (0.01, 0.7 and 7) were considered for an effect of the Prandtl number on natural convection. A two-dimensional solution for unsteady natural convection was obtained, using Chebyshev spectral methodology for different Rayleigh numbers varying over the range of $10^4$ to $10^6$. It had been experimentally and numerically reported [1,2] that the heat transfer mode becomes oscillatory when Pr is out of a specific Pr band beyond the critical Ra. In this study, we reproduced this phenomenon numerically. The variation of time- and surface-averaged Nusselt numbers on the hot and cold walls for different Rayleigh numbers and Prandtl numbers was presented to show the overall heat transfer characteristics in the system. And also, the isotherms and streamline distributions were presented in detail to compare the physics related to their thermal behavior.

초음파 분무 열분해법에 의한 ZnO 합성의 이론과 실제 (Theory and practice of synthesized ZnO powders by ultrasonic spray pyrolysis method)

  • 서수형;신건철
    • 한국결정성장학회지
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    • 제5권1호
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    • pp.60-66
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    • 1995
  • 초음파 분무기에 의해 분무된 질산아연 염($Zn(NO_3)_2$) 용액(0.5M)의 에어로졸 거동과 분포에 대한 실제 실험 결과는 computer simulation 결과와 일치하였다. 즉, 반응관(thermophoresis)에 의해 반응관 중심부로 이동하였다. 또한 에어로졸의 농도 분포는 축길이가 증가함에 따라 반응관 중심쪽에 높았다. 합성된 ZnO 입자 중에서 반응과 중심에서는 볼 수 없었던 깨진 형태의 shell-like aggregates가 반응관 벽근처에서 관찰되었으며, 입자의 크기는 반응관 벽쪽($ 1.2 {\mu\textrm{m}$)이 중심쪽($0.9 {\mu\textrm{m}$)보다 컸다.

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The Study of Corrosion Behavior of Active Screen Plasma Nitrided Stainless Steels

  • Chiu, L.H.;Chang, C.A.;Yeh, S.H.;Chen, F.S.;Chang, Heng
    • Corrosion Science and Technology
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    • 제6권5호
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    • pp.251-256
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    • 2007
  • Plasma nitriding is a surface treatment process which is increasingly used to improve wear, fatigue and corrosion resistance of industrial parts. Active screen plasma nitriding (ASPN) has both the advantages of the classic cold wall and the hot wall conventional dc plasma nitriding (DCPN) method and the parts to be nitrided are no longer directly exposed to the plasma. In this study, AS plasma nitriding has been used to nitride the UNS S31803 duplex stainless steel, AISI 304 and AISI 316 austenitic stainless steel, and AISI 420 martensitic stainless steel. Treated specimenswere characterized by means of microstructural analysis, microhardness measurements and electrochemical tests in NaCl aerated solutions. Hardness of the nitride cases of AISI 420 stainless steel by Knoop test can get up to 1300 HK0.1. From polarization tests, the corrosion current densities of AISI 420 and UNS S31803specimens ASPN at $420^{\circ}C$ were generally lower than those of their untreated substrates. The corrosion resistance of UNS S31803 duplex stainless steel can be enhanced by plasma nitriding at $420^{\circ}C$ Cowing to the formation of the S-phase.

소형 연소기 냉각 유로 개념 설계 (Conceptual Design of Coolant Channel for Sub-scale Combustion Chamber)

  • 정용현;조원국;한상엽;류철성
    • 한국추진공학회지
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    • 제6권4호
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    • pp.1-6
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    • 2002
  • 소형 연소기의 냉각 유로 설계를 위하여 열전달 및 냉각 유로의 구조해석을 수행하였다. 연소기의 고온가스에서의 열전달에 관한 2차원 해석을 수행하여 연소실 벽으로의 열유속을 예측한 다음 이를 3차원 해석을 위한 열경계 조건으로 적용하였다. 위 방법으로 예측한 열 유속은 기존의 경험식과 비교하여 검증하였으며 냉각수의 유량에 둔감한 것으로 판명되어 냉각 조건이 변화하더라도 동일한 열경계 조건을 사용할 수 있었다. 단일 냉각 유로에 대한 3차원 해석을 수행하여 연소실 벽의 최대온도 변화를 예측하였으며 이는 재사용 연소기 개발에 적용될 것이다. 냉각 유로의 정적 구조 해석을 통해 응력 분포와 구조 안전성을 예측하였다.

분말시스압연법에 의한 5 vol%CNT/Al 복합재료의 제조 및 평가 (Fabrication and Evaluation of 5 vol%CNT/Al Composite Material by a Powder in Sheath Rolling Method)

  • 홍동민;김우진;이성희
    • 한국재료학회지
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    • 제23권11호
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    • pp.607-612
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    • 2013
  • A powder in sheath rolling method was applied to the fabrication of a carbon nano tube (CNT) reinforced aluminum composite. A 6061 aluminum alloy tube with outer diameter of 31 mm and wall thickness of 2 mm was used as a sheath material. A mixture of pure aluminum powder and CNTs with a volume content of 5% was filled in the tube by tap filling and then processed to an 85% reduction using multi-pass rolling after heating for 0.5 h at $400^{\circ}C$. The specimen was then further processed at $400^{\circ}C$ by multi-pass hot rolling. The specimen was then annealed for 1 h at various temperatures that ranged from 100 to $500^{\circ}C$. The relative density of the 5vol%CNT/Al composite fabricated using powder in sheath rolling increased with increasing of the rolling reduction, becoming about 97% after hot rolling under 96 % total reduction. The relative density of the composite hardly changed regardless of the increasing of the annealing temperature. The average hardness also had only slight dependence on the annealing temperature. However, the tensile strength of the composite containing the 6061 aluminum sheath decreased and the fracture elongation increased with increasing of the annealing temperature. It is concluded that the powder in sheath rolling method is an effective process for fabrication of CNT reinforced Al matrix composites.

Hot wall epitaxy(HWE)법에 의한 $ZnIn_{2}Se_{4}$ 단결정 박막 성장과 가전자대 갈라짐에 대한 광전류 연구 (Photocurrent study on the splitting of the valence band and growth of $ZnIn_{2}Se_{4}$ single crystal thin film by hot wall epitaxy)

  • 홍광준
    • 한국결정성장학회지
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    • 제18권5호
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    • pp.217-224
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    • 2008
  • 수평 전기로에서 $ZnIn_2Se_4$ 단결정을 합성하여 HWE(Hot Wall Epitaxy)방법으로 $ZnIn_2Se_4$ 단결정 박막을 반절연성 GaAs(100) 기판에 성장시켰다. $ZnIn_2Se_4$ 단결정 박막의 성장 조건을 증발원의 온도 $630^{\circ}C$, 기판의 온도 $400^{\circ}C$였고 성장 속도는 0.5 $\mu m/hr$였다. $ZnIn_2Se_4$ 단결정 박막의 결정성의 조사에서 10K에서 광발광(photoluminescence) 스펙트럼이 682.7nm ($1.816{\underline{1}}eV$)에서 exciton emission 스펙트럼이 가장 강하게 나타났으며, 또한 이중결정 X-선 요통곡선(DCRC)의 반폭치(FWHM)도 128 arcsec로 가장 작아 최적 성장 조건임을 알 수 있었다. Hall 효과는 van der Pauw 방법에 의해 측정되었으며, 온도에 의존하는 운반자 농노와 이동도는 293 K에서 각각 $9.41\times10^{16}/cm^{-3}$, $292cm^2/V{\cdot}s$였다. $ZnIn_2Se_4$/SI(Semi-Insulated) GaAs(100) 단결정 박막의 광흡수와 광전류 spectra를 293 K에서 10K까지 측정하였다. 광흡수 스펙트럼으로부터 band gap $E_g(T)$는 varshni공식에 따라 계산한 결과 $E_g(T)=1.8622\;eV-(5.23\times10^{-4}eV/K)T^2/(T+775.5K)$ 이었으며 광전류 스펙트럼으로부터 Hamilton matrix(Hopfield quasicubic mode)법으로 계산한 결과 crystal field splitting energy ${\Delta}cr$값이 182.7meV이며 spin-orbit energy ${\Delta} so$값은 42.6meV임을 확인하였다. 10 K일 때 광전류 봉우리들은 n= 1, 27일때 $A_{1}-$, $B_{1}-$$C_{27}-exciton$ 봉우리임을 알았다.