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      곡관부 열전달 성능 강화를 위한 에어포일형 가이드 베인의 형상 최적설계

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      https://www.riss.kr/link?id=A60198236

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      다국어 초록 (Multilingual Abstract) kakao i 다국어 번역

      This paper presents the numerical simulation results of heat transfer and friction loss for a rotating two-pass duct with the airfoil-guide vanes in the turning region. The Kriging model is used as an optimization technique with Reynolds-averaged Navier-Stokes analysis of flow field and heat transfer with shear stress transport turbulent model. To improve the heat transfer performance, angle and location of the airfoil-guide vanes have been selected as design variables. The optimization problem has been defined as a minimization of the objective function, which is defined as a linear combination of heat transfer related term and friction loss related term with a weight factor. The airfoil-guide vanes in the turning region keep the high level of heat transfer while the friction loss has a low value. By comparing the presence or absence of airfoil-guide vanes, it is shown that the airfoil-guide vanes exhibited the best heat transfer performance to improve the blade cooling except the first passage.
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      This paper presents the numerical simulation results of heat transfer and friction loss for a rotating two-pass duct with the airfoil-guide vanes in the turning region. The Kriging model is used as an optimization technique with Reynolds-averaged Navi...

      This paper presents the numerical simulation results of heat transfer and friction loss for a rotating two-pass duct with the airfoil-guide vanes in the turning region. The Kriging model is used as an optimization technique with Reynolds-averaged Navier-Stokes analysis of flow field and heat transfer with shear stress transport turbulent model. To improve the heat transfer performance, angle and location of the airfoil-guide vanes have been selected as design variables. The optimization problem has been defined as a minimization of the objective function, which is defined as a linear combination of heat transfer related term and friction loss related term with a weight factor. The airfoil-guide vanes in the turning region keep the high level of heat transfer while the friction loss has a low value. By comparing the presence or absence of airfoil-guide vanes, it is shown that the airfoil-guide vanes exhibited the best heat transfer performance to improve the blade cooling except the first passage.

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      참고문헌 (Reference)

      1 Frank Zehnder, "The Effect of Turning Vanes on Pressure Loss and Heat Transfer of a Ribbed Rectangular Two-Pass Internal Cooling Channel" 2009

      2 김광용, "Optimization of a stepped circular pin-fin array to enhance heat transfer performance" SPRINGER-VERLAG 46 : 63-74, 200911

      3 김광용, "Multi-objective optimization of a cooling channel with staggered elliptic dimples" PERGAMON-ELSEVIER SCIENCE LTD 36 : 3419-3428, 201105

      4 Akira Murata, "Large Eddy Simulation with a Dynamic Subgrid-Scale Model of Turbulent Heat Transfer in an Orthogonally Rotating Rectangular Duct with Transverse Rib Turbulators" 47 : 1243-1259, 2000

      5 Kyung Min Kim, "Influence of Duct Aspect Ratio on Heat/Mass Transfer in Coolant Passages with Rotation" 28 : 357-373, 2007

      6 Liou T.-M., "Influence of Channel Aspect Ratio on Heat Transfer in Rotating Rectangular Ducts with Skewed Ribs at High Rotation Numbers" 42 : 5309-5322, 2009

      7 Wen-Lung Fu, "Heat Transfer in Two-Pass Rotating Rectangular Channels(AR=1:2 and AR=1:4) with 45-deg Angled Rib Turbulators" 127 : 165-174, 2005

      8 Gee D.L., "Forced Convection Heat Transfer in Helically Rib-Roughened Tubes" 23 : 1127-1136, 1980

      9 Mohammad Al-Qahtani, "Flow and Heat Transfer in Rotating Two-Pass Rectangular Channels (AR=2) by Reynolds Stress Turbulence Model" 45 : 1823-1838, 2002

      10 Iacovides H., "Experiments on Local Heat Transfer in a Rotating Square-Ended U-bend" 20 : 302-310, 1999

      1 Frank Zehnder, "The Effect of Turning Vanes on Pressure Loss and Heat Transfer of a Ribbed Rectangular Two-Pass Internal Cooling Channel" 2009

      2 김광용, "Optimization of a stepped circular pin-fin array to enhance heat transfer performance" SPRINGER-VERLAG 46 : 63-74, 200911

      3 김광용, "Multi-objective optimization of a cooling channel with staggered elliptic dimples" PERGAMON-ELSEVIER SCIENCE LTD 36 : 3419-3428, 201105

      4 Akira Murata, "Large Eddy Simulation with a Dynamic Subgrid-Scale Model of Turbulent Heat Transfer in an Orthogonally Rotating Rectangular Duct with Transverse Rib Turbulators" 47 : 1243-1259, 2000

      5 Kyung Min Kim, "Influence of Duct Aspect Ratio on Heat/Mass Transfer in Coolant Passages with Rotation" 28 : 357-373, 2007

      6 Liou T.-M., "Influence of Channel Aspect Ratio on Heat Transfer in Rotating Rectangular Ducts with Skewed Ribs at High Rotation Numbers" 42 : 5309-5322, 2009

      7 Wen-Lung Fu, "Heat Transfer in Two-Pass Rotating Rectangular Channels(AR=1:2 and AR=1:4) with 45-deg Angled Rib Turbulators" 127 : 165-174, 2005

      8 Gee D.L., "Forced Convection Heat Transfer in Helically Rib-Roughened Tubes" 23 : 1127-1136, 1980

      9 Mohammad Al-Qahtani, "Flow and Heat Transfer in Rotating Two-Pass Rectangular Channels (AR=2) by Reynolds Stress Turbulence Model" 45 : 1823-1838, 2002

      10 Iacovides H., "Experiments on Local Heat Transfer in a Rotating Square-Ended U-bend" 20 : 302-310, 1999

      11 Wei Chen, "Effect of Turning Vane Configurations on Heat Transfer and Pressure Drop in a Ribbed Internal Cooling System" 2010

      12 Ratna Rao D.V, "Effect of Turn Region Treatments on the Pressure Loss Distribution in a smooth Square Channel with Sharp 180° Bend" 10 : 459-468, 2004

      13 Sacks J, "Design and Analysis of Computer Experiments" 4 : 409-435, 1989

      14 Guoguang Su, "Computation of Flow and Heat Transfer in Rotating Two-Pass Rectangular Channels (AR=1:1, 1:2, and 1:4) with Smooth Walls by a Reynolds Stress Turbulence Model" 47 : 5665-5683, 2007

      15 Jiang Luo, "Analysis of Turbulent Flow in 180° Turning Ducts With and Without Guide Vanes" 131 : 2009

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      학술지 이력

      학술지 이력
      연월일 이력구분 이력상세 등재구분
      2027 평가예정 재인증평가 신청대상 (재인증)
      2021-01-01 평가 등재학술지 유지 (재인증) KCI등재
      2018-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2015-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2011-01-01 평가 등재 1차 FAIL (등재유지) KCI등재
      2009-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2006-01-01 평가 등재학술지 선정 (등재후보2차) KCI등재
      2005-06-16 학술지명변경 외국어명 : Jpurnal of Computatuonal Fluids Engineering -> Korean Society of Computatuonal Fluids Engineering KCI등재후보
      2005-01-01 평가 등재후보 1차 PASS (등재후보1차) KCI등재후보
      2004-01-01 평가 등재후보 1차 FAIL (등재후보1차) KCI등재후보
      2002-07-01 평가 등재후보학술지 선정 (신규평가) KCI등재후보
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      학술지 인용정보

      학술지 인용정보
      기준연도 WOS-KCI 통합IF(2년) KCIF(2년) KCIF(3년)
      2016 0.2 0.2 0.19
      KCIF(4년) KCIF(5년) 중심성지수(3년) 즉시성지수
      0.16 0.15 0.405 0.05
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