@inproceedings{eb3e6c1c04f84c83a64e6aecc4a8fd93,
title = "Limit cycle oscillations of swept-back wings in an incompressible flow",
abstract = "This study focuses on the limit cycle oscillations (LCO) of cantilever swept-back wings containing a cubic nonlinearity in an incompressible flow. The governing aeroelastic equations of two degrees-of-freedom swept wings are derived through applying the strip theory and unsteady aerodynamics. In order to apply strip theory, mode shapes of the cantilever beam are used. The harmonic balance method is used to calculate the frequencies of LCOs. Linear flutter analyses are conducted for several values of sweep angles to obtain the flutter boundaries.",
author = "S. Durmaz and Kaya, {M. O.}",
year = "2012",
language = "English",
isbn = "9781600869372",
series = "Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference",
booktitle = "53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference",
note = "53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference ; Conference date: 23-04-2012 Through 26-04-2012",
}