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Volume 36 Issue 2
Feb.  2010
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Journal of Beijing University of Aeronautics and Astronautics  > 2010  >  36(2): 218-222.
Luo Xiaoping, Huang Hai, Xian Kuichenget al. Vibration control design and simulation method for complex structures[J]. Journal of Beijing University of Aeronautics and Astronautics, 2006, 32(01): 18-21. (in Chinese)
Citation: Li Jian, Lee Chun-Hian, Jia Liping, et al. Numerical simulation on influencing parameter of micro-blowing technique[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(2): 218-222. (in Chinese)
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Numerical simulation on influencing parameter of micro-blowing technique

  • School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 13 Jan 2009
  • Publish Date: 28 Feb 2010
    Abstract
  • Taking micro-porous plates PN3 and PN23 of NASA Glenn Research Center as prototypes, four flat plates made of micro-channels aligning in single-, four-, eight- and sixteen-row patterns were chosen as the numerical models, and parametrical studies on skin friction reduction utilizing micro-blowing through micro-porous walls were performed for different geometric and physical parameters. Numerical results demonstrate that the velocity near the porous wall is decelerated by the micro-blowing, and thus affects the local skin friction distribution. The parametric studies also reveal the influences on the drag reduction capacities by various relevant parameters, which will provide some guidance on the application of micro-blowing technique (MBT) for drag deduction.

     

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  • [1] Hwang D P.Review of research into the concept of the microblowing technique for turbulent skin friction reduction[J].Progress in Aerospace Sciences,2004,40(8): 559-575 [2] Thiede P.Supercritical airfoil flow control by slot suction in shock region .AFFDL-TR-80-3088,1980 [3] Bahi L,Ross J M,Nagamatsu H T.Passive shock wave/boundary layer control for transonic airfoil drag reduction .AIAA-83-0137,1983 [4] Wood R M.Aerodynamic drag and drag reduction: energy and energy savings .AIAA-2003-209,2003 [5] Dershin H,Gallaher W H,Leonard C A.Direct measurement of skin friction on a porous flat plate with mass injection[J].AIAA Journal,1967,5(11):1934-1939 [6] Lin Y L,Chyu M K,Shih T I P,et al.Skin friction reduction through micro blowing .AIAA-98-0359,1998 [7] Hwang D P.Skin friction reduction by micro blowing technique:U S,5803410 ,1998-09-08 [8] Hwang D P.A proof of concept experiment for reducing skin friction by using a micro blowing technique .AIAA-97-0546,1997 [9] Hwang D P,Biesiadny T J.Experimental evaluation of the penalty associated with micro-blowing for reducing skin friction .AIAA-98-0677,1998 [10] Hwang D P.Skin-friction reduction by a micro-blowing technique [J].AIAA Journal,1998,36(3):480-481 [11] Hwang D P.An experimental study of turbulent skin friction reduction in supersonic flow using a microblowing technique .AIAA-2000-0545,2000 [12] Hwang D P.Experimental study of characteristics of micro-hole porous skins for turbulent skin friction reduction // 23rd International Congress of Aeronautical Sciences.Toronto,Canada:Elsevier Ltd,2002:2101.1-2101.7 [13] Li Jian,Lee Chun-Hian,Jia Liping,et al.Numerical study on flow control by micro-blowing .AIAA-2009-0779,2009 [14] Menter F R.Two-equation eddy-viscosity turbulence models for engineering applications[J].AIAA Journal,1994,32(8):1598-1605
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