2014
DOI: 10.12989/aas.2014.1.3.291
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Flutter analysis by refined 1D dynamic stiffness elements and doublet lattice method

Abstract: An advanced model for the linear flutter analysis is introduced in this paper. Higher-order beam structural models are developed by using the Carrera Unified Formulation, which allows for the straightforward implementation of arbitrarily rich displacement fields without the need of a-priori kinematic assumptions. The strong form of the principle of virtual displacements is used to obtain the equations of motion and the natural boundary conditions for beams in free vibration. An exact dynamic stiffness matrix i… Show more

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Cited by 6 publications
(2 citation statements)
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“…Varello et al (2013) extended the 1D CUF static aeroelastic formulation by exploiting a 3D panel aerodynamic method. Unsteady aeroelasticity for flutter analyses has been dealt with by Pagani et al (2014a) and Petrolo (2012Petrolo ( , 2013 through the Doublet Lattice Method (DLM). FEs and the DSM were employed to solve the aeroelastic problem.…”
Section: Aeroelasticitymentioning
confidence: 99%
“…Varello et al (2013) extended the 1D CUF static aeroelastic formulation by exploiting a 3D panel aerodynamic method. Unsteady aeroelasticity for flutter analyses has been dealt with by Pagani et al (2014a) and Petrolo (2012Petrolo ( , 2013 through the Doublet Lattice Method (DLM). FEs and the DSM were employed to solve the aeroelastic problem.…”
Section: Aeroelasticitymentioning
confidence: 99%
“…• Buckling [43], free vibration [44,45,46], dynamic response analysis [47] and aeroelasticity [48,49,50].…”
Section: Introductionmentioning
confidence: 99%