Abstract
The load analysis has highlighted the importance of an aerodynamic model able to describe not only the steady (or quasi-steady) effects of airfoil motion and flap deflection, but also the unsteady dynamics of the forces and moments, both in attached and stalled flow conditions. The model should also have low computational requirements to allow for an efficient integration with the BEM-based simulation environment of the aeroelastic code HAWC2, section 2.1.
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© 2014 Springer International Publishing Switzerland
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Bergami, L. (2014). ATEFlap Aerodynamic Model. In: Smart Rotor Modeling. Research Topics in Wind Energy, vol 3. Springer, Cham. https://doi.org/10.1007/978-3-319-07365-1_4
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DOI: https://doi.org/10.1007/978-3-319-07365-1_4
Publisher Name: Springer, Cham
Print ISBN: 978-3-319-07364-4
Online ISBN: 978-3-319-07365-1
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