Volume 12 Issue 1
Jan.  1997
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Article Navigation >  Journal of Aerospace Power  > 1997  >  12(1): 6-8,103
Xia Pinqi, Xu Guiqi. AN EXPERIMENTAL INVESTIGATION ON FLUTTER OF A HELICOPTER BLADE MODEL[J]. Journal of Aerospace Power, 1997, 12(1): 6-8,103.
Citation: Xia Pinqi, Xu Guiqi. AN EXPERIMENTAL INVESTIGATION ON FLUTTER OF A HELICOPTER BLADE MODEL[J]. Journal of Aerospace Power, 1997, 12(1): 6-8,103.
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AN EXPERIMENTAL INVESTIGATION ON FLUTTER OF A HELICOPTER BLADE MODEL

  • 1st Dept.Nanjing University of Aeronautics and Astronautics, Nanjing 210016

  • Received Date: 1996-02-01
  • Rev Recd Date: 1996-04-01
  • Publish Date: 1997-01-28
    Abstract
  • An experimental technique and method for flutter research of helicopter blade model are proposed.In the result of a series of experiments the relationships of blade flutter margin with rotor rotational speed,effective CG position of blade in chord and torsional stiffness of blade have been obtained.Some important conclusions have been reached.

     

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