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A Numerical Study on the Aerodynamics Effects of Time-Changing Wing Flexible Deformation in its Flapping Motions

  • BAO Lin ,
  • TONG Bing-Gang
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  • The Laboratory for Biomechanics of Animal Locomotion, Graduate School of the Chinese Academy of Sciences, Beijing 100049, China

Received date: 2004-12-15

  Revised date: 2005-01-13

  Online published: 2005-11-15

Abstract

A computational fluid dynamic study,based on 2-D incompressible Navier-Stokes Equations,is presented to investigate the aerodynamics effects of time-changing wing flexible deformation in its flapping.Two elementary motions of the wing flapping,i.e. accelerated translation and non-uniform rotation,are studied,in which both the flexible and rigid wing cases are compared.It is revealed that in comparison of the rigid wing case,the wing deformation acceleration in the flexible wing case leads to the added inertial effect,which causes a lot of change in instantaneous aerodynamic performance of the wing.With regard to the time-averaged one,the flexibility effect is much less.

Cite this article

BAO Lin , TONG Bing-Gang . A Numerical Study on the Aerodynamics Effects of Time-Changing Wing Flexible Deformation in its Flapping Motions[J]. Journal of University of Chinese Academy of Sciences, 2005 , 22(6) : 676 -684 . DOI: 10.7523/j.issn.2095-6134.2005.6.003

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