会议专题

Wake Signature and Strouhal Number Dependence of Finite-Span Flapping Wings

A numerical study was conducted in order to investigate the unsteady aerodynamics of finite-span flapping rigid wings. The unsteady laminar incompressible Navier-Stokes equations were solved on moving overlapping structured grids using a second-order accurate in space and time finite-difference scheme. Specifically, finite-span rigid wings undergoing pure heaving and root-flapping motions were studied. From the results presented, it is found that root-flapping wings produce wake structures similar to those of heaving wings, but with the difference that the latter wing kinematics generates larger vortices and forces than root-flapping wings; aside from this, similar wake regimes occur at comparable values of the Strouhal number. The numerical simulations were performed at a Reynolds number of Re=250 and at different values of Strouhal number and reduced frequency.

rolling wings overlapping grids wake signature vortex rings horseshoe shaped vortex thrust production

Joel E. Guerrero

University of Genoa, Via Montallegro 1, Genoa, 16145, Italy

国际会议

The 3rd International Conference of Bionic Engineering(第三届国际仿生工程会议ICBE10)

珠海

英文

109-122

2010-09-14(万方平台首次上网日期,不代表论文的发表时间)