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- W2323201580 abstract "The fluid mechanics of biomimetic airfoils and wings stands out as one of the most challenging areas of research to the scientific community. The basic underlying mechanisms are well known and have been established by early researchers through extensive experiments and numerical computations supported by classical theories of unsteady aerodynamics. Nevertheless, to date, experiments and numerical computations of this problem have been focused either on fluid mechanics alone or on fluid mechanics coupled with structural mechanics. The rigid body dynamics of plunging/pitching/flapping bodies has received less attention. In view of this, an attempt is made here to simulate the rigid body dynamics of plunging airfoils and wings in incompressible low Reynolds number flow in the range 10<Re<4.5x10 4 by solving the incompressible Navier-Stokes equations on moving overlapping meshes. The need for a sharp trailing edge is demonstrated by comparing the computed thrust and forward speed for airfoils with different trailing edge topologies when plunged in zero freestream velocity. The effect of freestream and ground proximity has also been analyzed for active flight. It is also shown that asymmetry of the leading and trailing edge is necessary for thrust production." @default.
- W2323201580 created "2016-06-24" @default.
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- W2323201580 date "2007-06-15" @default.
- W2323201580 modified "2023-10-16" @default.
- W2323201580 title "Numerical Study of Unsteady Low Reynolds Number Aerodynamics of Airfoils and Wings using Moving Overlapping Meshes" @default.
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- W2323201580 doi "https://doi.org/10.2514/6.2007-4559" @default.
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