High-fidelity aeroelastic computations of a flapping wing with spanwise flexibility

A high-order (up to 6th order) Navier–Stokes solver is coupled with a structural solver that decomposes the equations of three-dimensional elasticity into cross-sectional, small-deformation and spanwise, large-deformation analyses for slender wings. The resulting high-fidelity aeroelastic solver is...

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Veröffentlicht in:	Journal of fluids and structures 2013-07, Vol.40, p.86-104
Hauptverfasser:	Gordnier, Raymond E., Kumar Chimakurthi, Satish, Cesnik, Carlos E.S., Attar, Peter J.
Format:	Artikel
Sprache:	eng
Schlagworte:	Aeroelasticity Flapping wing Flexibility Flexible wings Mathematical analysis Micro air vehicle Navier-Stokes equations Plunging Solvers Unsteady aerodynamics Vortex dynamics Wings (aircraft)
Online-Zugang:	Volltext
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