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      플라즈마 가진에 의한 원형 실린더 후류의 제어

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      https://www.riss.kr/link?id=A60198268

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      다국어 초록 (Multilingual Abstract) kakao i 다국어 번역

      Numerical simulations are carried out for flow over a circular cylinder controlled by the momentum forcing which is generated by a pair of plasma actuators symmetrically mounted on the cylinder surface. A popular and empirical plasma model is used for the spatial distribution of momentum forcing. In this study, we consider two different types of actuation, i.e., steady and unsteady (or pulsed) actuation. In the unsteady actuation, the actuation is turned on and off periodically, its frequency being a control parameter. The objective of this study is to investigate the effects of actuator location and actuation frequency on the flow structures and the forces on the cylinder. Results show that the cylinder wake can be effectively controlled by proper actuator location. For example, when the actuators are located at 120° from the stagnation point, vortex shedding is completely suppressed with the boundary layer almost fully attached to the surface, resulting in drag reduction and lift elimination.
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      Numerical simulations are carried out for flow over a circular cylinder controlled by the momentum forcing which is generated by a pair of plasma actuators symmetrically mounted on the cylinder surface. A popular and empirical plasma model is used for...

      Numerical simulations are carried out for flow over a circular cylinder controlled by the momentum forcing which is generated by a pair of plasma actuators symmetrically mounted on the cylinder surface. A popular and empirical plasma model is used for the spatial distribution of momentum forcing. In this study, we consider two different types of actuation, i.e., steady and unsteady (or pulsed) actuation. In the unsteady actuation, the actuation is turned on and off periodically, its frequency being a control parameter. The objective of this study is to investigate the effects of actuator location and actuation frequency on the flow structures and the forces on the cylinder. Results show that the cylinder wake can be effectively controlled by proper actuator location. For example, when the actuators are located at 120° from the stagnation point, vortex shedding is completely suppressed with the boundary layer almost fully attached to the surface, resulting in drag reduction and lift elimination.

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      참고문헌 (Reference)

      1 Williamson, D, "The response and symmetry properties of a cylinder wake subjected to localized surface excitation" 234 : 71-96, 1992

      2 Glezer, A., "Synthetic jets" 34 : 503-529, 2002

      3 Post, M.L., "Separation control on high angle of attack airfoil using plasma actuators" 42 : 2177-2184, 2004

      4 Kozlov, A, "Plasma flow control of cylinders in a tandem configuration" 49 : 2183-2193, 2011

      5 Thomas, F.O, "Plasma actuators for cylinder flow control and noise reduction" 46 : 1921-1931, 2008

      6 Williamson, C.H.K, "Oblique and parallel modes of vortex shedding in the wake of a circular cylinder at low Reynolds numbers" 206 : 579-627, 1989

      7 Park, C, "Numerical solutions of flow past a circular cylinder at Reynolds numbers up to 160" 12 : 1200-1205, 1998

      8 Shyy, W, "Modeling of glow discharge-induced fluid dynamics" 92 : 6434-6443, 2002

      9 Kim, D, "Large-eddy simulation of flow over a circular cylinder with plasma-based control" 2009

      10 Rizzetta, D.P., "Large eddy simulation of plasma-based control strategies for bluff body flow" 47 : 717-729, 2009

      1 Williamson, D, "The response and symmetry properties of a cylinder wake subjected to localized surface excitation" 234 : 71-96, 1992

      2 Glezer, A., "Synthetic jets" 34 : 503-529, 2002

      3 Post, M.L., "Separation control on high angle of attack airfoil using plasma actuators" 42 : 2177-2184, 2004

      4 Kozlov, A, "Plasma flow control of cylinders in a tandem configuration" 49 : 2183-2193, 2011

      5 Thomas, F.O, "Plasma actuators for cylinder flow control and noise reduction" 46 : 1921-1931, 2008

      6 Williamson, C.H.K, "Oblique and parallel modes of vortex shedding in the wake of a circular cylinder at low Reynolds numbers" 206 : 579-627, 1989

      7 Park, C, "Numerical solutions of flow past a circular cylinder at Reynolds numbers up to 160" 12 : 1200-1205, 1998

      8 Shyy, W, "Modeling of glow discharge-induced fluid dynamics" 92 : 6434-6443, 2002

      9 Kim, D, "Large-eddy simulation of flow over a circular cylinder with plasma-based control" 2009

      10 Rizzetta, D.P., "Large eddy simulation of plasma-based control strategies for bluff body flow" 47 : 717-729, 2009

      11 Kim, J., "Distributed forcing of flow over a circular cylinder" 17 : 1-16, 2005

      12 Corke, T.C, "Dielectric barrier discharge plasma actuators for flowcontrol" 42 : 505-529, 2010

      13 Moreau, E, "Airflow control by non-thermal plasma actuators" 40 : 605-636, 2007

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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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