Cesnik, CES

Palacios, R

English

A low-order aeroelastic model is introduced for very flexible high-aspect-ratio wings with adaptive airfoils. A geometrically-nonlinear beam-like model capable of capturing plate-like deformations has been coupled with a 2-D finite-state aerodynamic model with arbitrary airfoil deformations. The proposed approach results in a natural extension to the conventional way of analyzing high-aspect-ratio wings, with very little additional complexity. The control effectiveness of camber deformation is numerically investigated in some simple situations, including thin isotropic and anisotropic plates and a straight wing with a constant NACA4406 airfoil

Rafael Palacios

Carlos E. S. Cesnik

CiteSeerX

Low-speed aeroelastic modeling of very flexible slender wings with deformable airfoils

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76763/1/AIAA-2008-1995-728.pd

Palacios, Rafael

Cesnik, Carlos E. S.

Deep Blue Documents

Low-Speed Aeroelastic Modeling of Very Flexible Slender Wings with Deformable Airfoils

Carlos Cesnik

Crossref

Spiral - Imperial College Digital Repository

http://deepblue.lib.umich.edu/bitstream/2027.42/76763/1/AIAA-2008-1995-728.pdf

Low-Speed Aeroelastic Modeling of Very Flexible Slender Wings with Deformable Airfoils

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CiteSeerX

Deep Blue Documents

Crossref

Spiral - Imperial College Digital Repository