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      https://www.riss.kr/link?id=A99760021

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      다국어 초록 (Multilingual Abstract)

      Effect of semicircular rib or groove on the performance of a rim-seal was evaluated using three-dimensional Reynolds-averaged Navier-Stokes equations. The turbulence was modeled using the one-equation Spalart-Allmaras turbulence closure model. Reynolds number based on the axial chord of the turbine blade was 500,000 at the mainstream outlet. The numerical results for a sealing effectiveness was validated in comparison with experimental data. To examine the effect of the semicircular rib or groove on sealing effectiveness of the rim-seal, location and diameter of the rib or groove were selected as the parameters to be performed. The rim-seals with the semicircular groove showed a higher sealing effectiveness than that with the semicircular rib. The semicircular groove installed on the stator side showed best sealing effectiveness among the numerical simulation results.
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      Effect of semicircular rib or groove on the performance of a rim-seal was evaluated using three-dimensional Reynolds-averaged Navier-Stokes equations. The turbulence was modeled using the one-equation Spalart-Allmaras turbulence closure model. Reynold...

      Effect of semicircular rib or groove on the performance of a rim-seal was evaluated using three-dimensional Reynolds-averaged Navier-Stokes equations. The turbulence was modeled using the one-equation Spalart-Allmaras turbulence closure model. Reynolds number based on the axial chord of the turbine blade was 500,000 at the mainstream outlet. The numerical results for a sealing effectiveness was validated in comparison with experimental data. To examine the effect of the semicircular rib or groove on sealing effectiveness of the rim-seal, location and diameter of the rib or groove were selected as the parameters to be performed. The rim-seals with the semicircular groove showed a higher sealing effectiveness than that with the semicircular rib. The semicircular groove installed on the stator side showed best sealing effectiveness among the numerical simulation results.

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      참고문헌 (Reference)

      1 Popović, I., "The Effect on Unsteadiness and Compressibility on the Interaction between Hub Leakage And Mainstream Flows in HP Turbines" 2011

      2 Lynch, S. P., "The Effect of Combustor-turbine Interface Gap Leakage on the Endwall Heat Transfer for a Nozzle Guide Vane" 2007

      3 Popović, I., "Improving Turbine Stage Efficiency and Sealing Effectiveness through Modification of the Rim Seal Geometry" 2012

      4 Deck, S., "Development and Application of Spalart-Allamaras One Equation Turbulence Model to Three-Dimensional Supersonic Complex Configurations" 6 : 171-183, 2002

      5 Wang, C. Z., "Comparison of Flow Characteristics in Axial-gap Seals for Close-and Wide-spaced Turbine Stages" 2007

      6 Popović, I., "Aerothermal Impact of the Interaction between Hub Leakage and Mainstream Flows in Highly-loaded HP Turbine Blades" 2010

      7 "ANSYS CFX-11.0, Solver Theory" Ansys Inc. 2006

      8 Spalart, P. R., "A One-Equation Turbulence Model for Aerodynamic Flows" AIAA, Aerospace Sciences Meeting and Exhibit 1992

      1 Popović, I., "The Effect on Unsteadiness and Compressibility on the Interaction between Hub Leakage And Mainstream Flows in HP Turbines" 2011

      2 Lynch, S. P., "The Effect of Combustor-turbine Interface Gap Leakage on the Endwall Heat Transfer for a Nozzle Guide Vane" 2007

      3 Popović, I., "Improving Turbine Stage Efficiency and Sealing Effectiveness through Modification of the Rim Seal Geometry" 2012

      4 Deck, S., "Development and Application of Spalart-Allamaras One Equation Turbulence Model to Three-Dimensional Supersonic Complex Configurations" 6 : 171-183, 2002

      5 Wang, C. Z., "Comparison of Flow Characteristics in Axial-gap Seals for Close-and Wide-spaced Turbine Stages" 2007

      6 Popović, I., "Aerothermal Impact of the Interaction between Hub Leakage and Mainstream Flows in Highly-loaded HP Turbine Blades" 2010

      7 "ANSYS CFX-11.0, Solver Theory" Ansys Inc. 2006

      8 Spalart, P. R., "A One-Equation Turbulence Model for Aerodynamic Flows" AIAA, Aerospace Sciences Meeting and Exhibit 1992

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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
      2014-01-08 학회명변경 영문명 : Korean Fluid Machinery Association -> Korean Society for Fluid Machinery KCI등재
      2014-01-08 학술지명변경 외국어명 : 미등록 -> The KSFM Journal of Fluid Machinery KCI등재
      2013-01-09 학회명변경 한글명 : 유체기계공업학회 -> 한국유체기계학회 KCI등재
      2013-01-09 학술지명변경 한글명 : 유체기계저널 -> 한국유체기계학회 논문집 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
      2005-01-01 평가 등재후보 1차 PASS (등재후보1차) KCI등재후보
      2004-01-01 평가 등재후보학술지 유지 (등재후보1차) KCI등재후보
      2003-01-01 평가 등재후보학술지 선정 (신규평가) KCI등재후보
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      학술지 인용정보

      학술지 인용정보
      기준연도 WOS-KCI 통합IF(2년) KCIF(2년) KCIF(3년)
      2016 0.32 0.32 0.29
      KCIF(4년) KCIF(5년) 중심성지수(3년) 즉시성지수
      0.25 0.23 0.601 0.04
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