4.7 Article

Effect of wing inertia on hovering performance of flexible flapping wings

Journal

PHYSICS OF FLUIDS
Volume 22, Issue 11, Pages -

Publisher

AMER INST PHYSICS
DOI: 10.1063/1.3499739

Keywords

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Funding

  1. NSF [CBET-0954381]
  2. Div Of Chem, Bioeng, Env, & Transp Sys
  3. Directorate For Engineering [954381] Funding Source: National Science Foundation

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Insect wings in flight typically deform under the combined aerodynamic force and wing inertia, whichever is dominant depends on the mass ratio defined as m*=rho(s)h/(rho(f)c), where rho(s)h is the surface density of the wing, rho(f) is the density of the air, and c is the characteristic length of the wing To study the differences that the wing inertia makes in the aerodynamic performance of the deformable wing, a two-dimensional numerical study is applied to simulate the flow-structure interaction of a flapping wing during hovering flight The wing section is modeled as an elastic plate, which may experience nonlinear deformations while flapping The effect of the wing inertia on lift production, drag resistance, and power consumption is studied for a range of wing rigidity It is found that both inertia-induced deformation and flow-induced deformation can enhance lift of the wing However, the flow-induced deformation, which corresponds to the low-mass wing, produces less drag and leads to higher aerodynamic power efficiency In addition, the wing deformation has a significant effect on the unsteady vortices around the wing The implication of the findings on insect flight is discussed (C) 2010 American Institute of Physics [dot 10.1063/1.3499739]

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