@inproceedings{9988c0fb1b8a44bfa2a61cbb5651af71,
title = "Nonlinear X-DIA wing response to the oscillations of a control surface",
abstract = "The ability to model nonlinear wing/control surface relations is an essential component for the design and implementation of nonlinear control laws that make use of control surfaces and exploit these relations. In this work, an experimental investigation is conducted to determine nonlinear wing response to the oscillations of a control surface of an aeroelastic demonstrator. Higher-order spectral moments are applied to Identify quadratic and cubic nonlinearities. The results show enhanced response of the wing at the excitation frequency. Additionally, the wing's response is characterized by quadratic and cubic nonlinearities.",
author = "Alessandro Scotti and Sergio Ricci and Hajj, \{Muhammad R.\}",
year = "2007",
doi = "10.2514/6.2007-2133",
language = "English",
isbn = "1563478927",
series = "Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
pages = "5192--5199",
booktitle = "Collection of Technical Papers - 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference",
note = "48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference ; Conference date: 23-04-2007 Through 26-04-2007",
}