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Volume 27 Issue 1
Jan.  2001
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Journal of Beijing University of Aeronautics and Astronautics  > 2001  >  27(1): 54-56.
SHEN Xia-ling, WANG Li-li. Aerodynamic Analysis of Grid Fin-Body Configurations[J]. Journal of Beijing University of Aeronautics and Astronautics, 2001, 27(1): 54-56. (in Chinese)
Citation: SHEN Xia-ling, WANG Li-li. Aerodynamic Analysis of Grid Fin-Body Configurations[J]. Journal of Beijing University of Aeronautics and Astronautics, 2001, 27(1): 54-56. (in Chinese)
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Aerodynamic Analysis of Grid Fin-Body Configurations

  • Beijing University of Aeronautics and Astronautics, Dept. of Flight Vehicle Design and Applied Mechanics

  • Received Date: 26 Aug 1999
  • Publish Date: 31 Jan 2001
    Abstract
  • Aerodynamic analysis is made for grid fin-body configurations in subsonic and supersonic flow. Vortex lattice formulation has been used in predicting the aerodynamic characteristics for grid fin in subsonic flow. An infinite line doublet and imaging vortices inside the body are employed to model body upward and wing-body carry over load.In supersonic flow, the grid fin is assumed to locate in the cross flow of the body, the wing panel theory is used for calculating the aerodynamic interfere factor of the grid fin produced by the body. The aerodynamic characteristics of some grid fin-body configurations have been calculated, the theory agreed quite well with the experimental data.

     

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  • [1] Белочерковското　С　М.Решетчатые　крылъя[M]．Москва:Машиностроение,1985. [2] Brooks R A, Burkhalter E B. Experimental and analytical analysis of grid fin configurations . AIAA-88-0280,1988． [3] Burkhalter E B.Grid fin aerodynamics for missile applications in supersonic flow[J].Journal of Spacecraft and Rockets,1996,33(1):38~41. [4] 陆中荣,沈遐龄,童自力,等.栅格翼空气动力特性的计算与分析[J].北京航空航天大学学报,1996,22(5):575~580. [5] 沈遐龄,陆中荣,童自力,等.栅格翼机身发动机组合体气动特性计算[J]．北京航空航天大学学报,1996,22(6):727~732． [6] Auman L.Aerodynamic data base user-s guide . US Army Report TR-RD-SS-92-77,1977.
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