Nonlinear mechanics and finite element with material damping for the static and dynamic analysis of composite wind turbine blades

• Κύριος συγγραφέας: Χόρτης, Δημήτριος
• Άλλοι συγγραφείς: Σαραβάνος, Δημήτριος
• Μορφή: Thesis
• Γλώσσα: English
• Έκδοση: 2012
• Θέματα: Nonlinear damping; Composites beams; Wind turbine blades; Nonlinear finite elements; Membrane stiffening; Buckling; Material coupling; Geometric nonlinearities due to large deformations; Μη-γραμμική απόσβεση; Δοκοί από σύνθετα υλικά; Πτερύγια ανεμογεννητριών; Μη-γραμμικά πεπερασμένα στοιχεία; Δυσκαμψία; Λυγισμός και μεταλυγισμός δοκών από σύνθετα υλικά; Σύζευξη λόγω χρήσης συνθέτων υλικών; Γραμμική μη-γραμμικότητα λόγω μεγάλων παραμορφώσεων; 624.171

The aim of the current dissertation is the development of finite element models capable of predicting the damping and the damped structural dynamic response of laminated composite blades and beams. The present thesis is divided into two main parts, of which the first one studies the material coupling effect on the static and modal characteristics of composite structures. New damping coupling terms are formulated and incorporated into a linear beam finite element to better capture the composite material and structural coupling effects. The second part describes the theoretical framework for predicting the nonlinear damping and damped vibration of laminated composite structures due to large in-plane tensile and compressive forces. A nonlinear beam finite element for composite strips is developed capable of capturing the effects of geometric nonlinearity on the damping of composite laminates. The damping mechanics consider a strain based Kelvin viscoelastic model and Green-Lagrange nonlinear strain expressions, which introduce geometric nonlinearity into the formulation. Incorporation of first-order shear deformation theory into the equations of motion provides the linear and new nonlinear cross-section stiffness and damping terms. Within each element, the stain field is approximated by linear interpolation shape functions. An incremental-iterative methodology is formulated into the finite element solver, based on the Newton-Raphson technique in order to obtain the system solution at each iteration, till the final convergence is achieved. For the sake of completeness, a series of experimental measurements were carried out for the composite strip, subject to tensile and buckling loads. Correlations with theoretical predictions gave credence to the ability of the nonlinear finite element to predict damping of composite structures undergoing large displacements and rotations in the nonlinear regime. The finite element was further extended to include the nonlinear analysis of large-scale hollow composite structures. New first- and second-order stiffness and damping terms were developed and incorporated into an updated nonlinear beam finite element, capable of capturing the effect of rotational stresses on the static and modal characteristics of composite beams and blades.