LIU Xin-jian, YUAN Tian-bao. Effects of Unsteady Deformation of a Flapping Wing on Its Aerodynamic Forces[J]. Applied Mathematics and Mechanics, 2008, 29(6): 663-675.
Citation: LIU Xin-jian, YUAN Tian-bao. Effects of Unsteady Deformation of a Flapping Wing on Its Aerodynamic Forces[J]. Applied Mathematics and Mechanics, 2008, 29(6): 663-675.

Effects of Unsteady Deformation of a Flapping Wing on Its Aerodynamic Forces

  • Received Date: 2007-01-17
  • Rev Recd Date: 2008-04-17
  • Publish Date: 2008-06-15
  • The effects of unsteady deformation of a flapping model insect wing on its aero dynamic force production were studied by solving the Navier-Stokes equations on a dynamically deforming grid. Aerodynamic forces on the flapping wing are little affected by consider abletwist, but are affected by camber deformation; the effect of combined camber and twist deformation is similar to that of camber deformation. With a de formation of 6% camber and 20 degrees twist (typical values observed forwings of many insects), lift is increased by 10~20% and lift-to-dragratio by around 10% compared with the case of rigid flat-plate wing. As a result, the deformation canincrease the maximum lift coefficient of aninsect, and candecrease its power requirement of flight, e. g., for a hovering bumblebee with dynamically deforming wings (6% camber and 20 degrees twist), aerodynamic power required is de creased by about 16% compared with the case of rigid wings.
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