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      다국어 초록 (Multilingual Abstract) kakao i 다국어 번역

      In this paper, we study the effect of various turbulence models by comparing the aerodynamic characteristics and the flow patterns computed for aircraft models. An in-house CFD solver, MSAPv, that solves the three dimensional RANS equations with the turbulence model equations is used. The turbulence models used in this study are the Spalart-Allmaras model, Menters k-w SST model, Coakleys q-w model, and Huang and Coakleys k-emodel. DLR-F6 WB and WBNP configurations are selected for the study. We concentrate on the separated flow pattern variations with the turbulence models at the wing-body junction and the wing-pylon junction as well as drag polar curves.
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      In this paper, we study the effect of various turbulence models by comparing the aerodynamic characteristics and the flow patterns computed for aircraft models. An in-house CFD solver, MSAPv, that solves the three dimensional RANS equations with the t...

      In this paper, we study the effect of various turbulence models by comparing the aerodynamic characteristics and the flow patterns computed for aircraft models. An in-house CFD solver, MSAPv, that solves the three dimensional RANS equations with the turbulence model equations is used. The turbulence models used in this study are the Spalart-Allmaras model, Menters k-w SST model, Coakleys q-w model, and Huang and Coakleys k-emodel. DLR-F6 WB and WBNP configurations are selected for the study. We concentrate on the separated flow pattern variations with the turbulence models at the wing-body junction and the wing-pylon junction as well as drag polar curves.

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      참고문헌 (Reference)

      1 Menter, F. R., "Two-equation eddy-viscosity turbulence models for engineering applications" 32 (32): 1598-1605, 1994

      2 Coakley, T. J., "Turbulence modeling methods for the compressible Navier-Stokes equations" AIAA 1983

      3 Van Leer, B., "Towards the ultimate conservative difference scheme. II. Monotonicity and conservation combined in a second-order scheme" 14 (14): 361-370, 1974

      4 Laflin, K., "Summary of Data from the Second AIAA CFD Drag Prediction Workshop(Invited)" 2004

      5 Schmitt, V., "Pressure Distributions on the ONERA-M6-Wing at Transonic Mach Numbers" 1979

      6 곽인근, "Performance Evaluation of Two-Equation Turbulence Models for 3D Wing-Body Configuration" 한국항공우주학회 13 (13): 307-316, 2012

      7 Lee, S., "On coupling the Reynolds averaged Navier Stokes equations with two equation turbulence model equations" 50 (50): 165-197, 2006

      8 Beam, R. M., "Implicit numerical methods for the compressible Navier-Stokes and Euler equations" Von Karman Institute for Fluid Dynamics Lecture Series 1982

      9 Tinoco, E., "Drag prediction with the Zeus/CFL3D system" 2004

      10 May, G., "Drag prediction of the DLR-F6 configuration" AIAA 2004

      1 Menter, F. R., "Two-equation eddy-viscosity turbulence models for engineering applications" 32 (32): 1598-1605, 1994

      2 Coakley, T. J., "Turbulence modeling methods for the compressible Navier-Stokes equations" AIAA 1983

      3 Van Leer, B., "Towards the ultimate conservative difference scheme. II. Monotonicity and conservation combined in a second-order scheme" 14 (14): 361-370, 1974

      4 Laflin, K., "Summary of Data from the Second AIAA CFD Drag Prediction Workshop(Invited)" 2004

      5 Schmitt, V., "Pressure Distributions on the ONERA-M6-Wing at Transonic Mach Numbers" 1979

      6 곽인근, "Performance Evaluation of Two-Equation Turbulence Models for 3D Wing-Body Configuration" 한국항공우주학회 13 (13): 307-316, 2012

      7 Lee, S., "On coupling the Reynolds averaged Navier Stokes equations with two equation turbulence model equations" 50 (50): 165-197, 2006

      8 Beam, R. M., "Implicit numerical methods for the compressible Navier-Stokes and Euler equations" Von Karman Institute for Fluid Dynamics Lecture Series 1982

      9 Tinoco, E., "Drag prediction with the Zeus/CFL3D system" 2004

      10 May, G., "Drag prediction of the DLR-F6 configuration" AIAA 2004

      11 Roe, P. L., "Approximate Riemann solvers, parameter vectors, and difference schemes" 43 (43): 357-372, 1981

      12 Huang, P. G., "An implicit Navier-Stokes code for turbulent flow modeling" AIAA 1992

      13 Spalart, P. R., "A One-Equation Turbulence Model for Aerodynamic Flows" AIAA 1992

      14 "2nd AIAA CFD Drag Prediction Workshop" AIAA

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      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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      2016 0.2 0.2 0.19
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      0.16 0.15 0.405 0.05
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