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      https://www.riss.kr/link?id=A76320935

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      다국어 초록 (Multilingual Abstract) kakao i 다국어 번역

      This research computes the viscous flow field and aerodynamics around the model of a commercial passenger airplane, Boeing 747-400, which cruises in transonic speed. The configuration was realized through the reverse engineering based on the photo scanning measurement. In results, the pressure coefficients at the several wing section on the wing surface of the airplane was described and discussed to obtain the physical meaning. The lift coefficient increased almost linearly up to 17°. Here the maximum lift occurred at 18° according to the angle of attack And the minimum drag is expected at -2°. The maximum lift coefficient occurred at the Mach number 0.89, and the drag coefficient rapidly increased after the Mach number of 0.92. Also shear-stress transport model predicts slightly lower aerodynamic coefficients than other models and Chen’s model shows the highest aerodynamic values. The aerodynamic performance of the airplane elements was presented.
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      This research computes the viscous flow field and aerodynamics around the model of a commercial passenger airplane, Boeing 747-400, which cruises in transonic speed. The configuration was realized through the reverse engineering based on the photo sca...

      This research computes the viscous flow field and aerodynamics around the model of a commercial passenger airplane, Boeing 747-400, which cruises in transonic speed. The configuration was realized through the reverse engineering based on the photo scanning measurement. In results, the pressure coefficients at the several wing section on the wing surface of the airplane was described and discussed to obtain the physical meaning. The lift coefficient increased almost linearly up to 17°. Here the maximum lift occurred at 18° according to the angle of attack And the minimum drag is expected at -2°. The maximum lift coefficient occurred at the Mach number 0.89, and the drag coefficient rapidly increased after the Mach number of 0.92. Also shear-stress transport model predicts slightly lower aerodynamic coefficients than other models and Chen’s model shows the highest aerodynamic values. The aerodynamic performance of the airplane elements was presented.

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      참고문헌 (Reference)

      1 Marvin, P.F, "Wind-tunnel tests of a full-scale model of a light twin-engine airplane with fixed auxiliary airfoil or leading-edge slot" 1974

      2 Bardina, J.E., "Turbulence modeling validation" 1997

      3 Boppe, C.W., "Transonic flow field analysis for wing-fuselage configurations" 1980

      4 Lee-Rausch, E.M., "Transonic drag prediction on a DLR-F6 transport configuration using unstructured grid solvers" 2004

      5 McCroskey, W.L., "The Phenomenon of dynamic stall" 1981

      6 David, W.L. et al., "Summary of data from the firs AIAA CFD drag prediction workshop" 2002

      7 Rumsey, C.L., "Study of CFD Variation on transport configurations from the second drag-prediction workshop" 2004

      8 Jou, W.H., "Practical considerations in aerodynamic design optimization" 1995

      9 Johnson, W., "On the mechanism of dynamic stall" 17 : 36-45, 1972

      10 Vos, J.B., "Navier-Stokes solvers in European aircraft design" 38 : 601-697, 2002

      1 Marvin, P.F, "Wind-tunnel tests of a full-scale model of a light twin-engine airplane with fixed auxiliary airfoil or leading-edge slot" 1974

      2 Bardina, J.E., "Turbulence modeling validation" 1997

      3 Boppe, C.W., "Transonic flow field analysis for wing-fuselage configurations" 1980

      4 Lee-Rausch, E.M., "Transonic drag prediction on a DLR-F6 transport configuration using unstructured grid solvers" 2004

      5 McCroskey, W.L., "The Phenomenon of dynamic stall" 1981

      6 David, W.L. et al., "Summary of data from the firs AIAA CFD drag prediction workshop" 2002

      7 Rumsey, C.L., "Study of CFD Variation on transport configurations from the second drag-prediction workshop" 2004

      8 Jou, W.H., "Practical considerations in aerodynamic design optimization" 1995

      9 Johnson, W., "On the mechanism of dynamic stall" 17 : 36-45, 1972

      10 Vos, J.B., "Navier-Stokes solvers in European aircraft design" 38 : 601-697, 2002

      11 Alister, K.W., "Dynamic stall experiments on the NACA0012 airfoils" 1978

      12 McCroskey, W.L., "Dynamic stall experiments on oscillating airfoils" 14 : 57-63, 1976

      13 George, S.D., "Dynamic stall experiments on oscillating airfoils" 13 : 1354-1359, 1975

      14 Martin, G., "Comparison of aerodynamic performance of raked wing tips and large winglets" Cranfield university 2006

      15 Asley, H., "Aerodynamics of wings and bodies, Reading" Addison-Wesley Publishing Co. 1965

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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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