Show/Hide Menu
Hide/Show Apps
Logout
Türkçe
Türkçe
Search
Search
Login
Login
OpenMETU
OpenMETU
About
About
Open Science Policy
Open Science Policy
Open Access Guideline
Open Access Guideline
Postgraduate Thesis Guideline
Postgraduate Thesis Guideline
Communities & Collections
Communities & Collections
Help
Help
Frequently Asked Questions
Frequently Asked Questions
Guides
Guides
Thesis submission
Thesis submission
MS without thesis term project submission
MS without thesis term project submission
Publication submission with DOI
Publication submission with DOI
Publication submission
Publication submission
Supporting Information
Supporting Information
General Information
General Information
Copyright, Embargo and License
Copyright, Embargo and License
Contact us
Contact us
Classical Aeroelastic Stability Analysis of Large Composite Wind Turbine Blades
Date
2016-01-04
Author
Farsadi, Touraj
Kayran, Altan
Metadata
Show full item record
Item Usage Stats
206
views
0
downloads
Cite This
To achieve higher energy production bigger wind turbine systems with very long blades are increasingly used in the wind turbine industry. As the length of the wind turbine blades is increased, blades become more flexible in bending and torsion. Increased bending and torsional flexibility of long wind turbine blades may cause torsional divergence and flapwise bending-torsion flutter at high speeds. Therefore, it is important that aeroelastic stability characteristics of the blades be investigated to ensure that wind turbine system is free of any aeroelastic instability. In this study, classical aeroelastic stability approach is applied to a simplified composite blade model. For the purpose of the study, the composite wind turbine blade is modeled as an elastic cantilevered rotating thin-walled composite box beam with the developed Circumferentially Asymmetric Stiffness (CAS) structural model. Circumferentially asymmetric stiffness structural model takes into account a group of non-classical effects such as the transverse shear, the material anisotropy and warping restraint. The aerodynamic strip method based on indicial function in unsteady incompressible flow is used to simulate incompressible unsteady aerodynamic effects. Hamilton’s principle and the extended Galerkin’s method are used to obtain the coupled linear governing system of dynamic equations. Preliminary results show that fiber angle of the CAS structural model affects the aeroelastic instability speed significantly and fiber angle also controls the aeroelastic instability mode.
URI
http://arc.aiaa.org/series/6.scitech
https://hdl.handle.net/11511/73529
DOI
https://doi.org/10.2514/6.2016-1959
Conference Name
AIAA Science and Technology Forum and Exposition
Collections
Department of Aerospace Engineering, Conference / Seminar
Suggestions
OpenMETU
Core
Structural Performance and Power Production of Wind Turbine Systems with Bend-Twist Coupled Blades in Underrated Wind Conditions
Şener, Özgün; Kayran, Altan (2018-01-12)
The implementation of bend-twist coupling effect on wind turbine blades on the structural performance and power production of wind turbine system exposed to underrated wind conditions are studied. The structural performance of wind turbine systems are evaluated by the decrease in damage equivalent loads in the whole wind turbine system and reduction in maximum fiber direction stresses in the blades with the exploitation of off-axis plies in the main spar caps of the wind turbine blades. Wind turbine models ...
Delamination-Debond Behaviour of Composite T-Joints in Wind Turbine Blades
Gulasik, H.; Çöker, Demirkan (2014-06-20)
Wind turbine industry utilizes composite materials in turbine blade structural designs because of their high strength/stiffness to weight ratio. T-joint is one of the design configurations of composite wind turbine blades. T-joints consist of a skin panel and a stiffener co-bonded or co-cured together with a filler material between them. T-joints are prone to delaminations between skin/stiffener plies and debonds between skin-stiffener-filler interfaces. In this study, delamination/debond behavior of a co-b...
Preliminary study on the applicability of semi-geodesic winding in the design and manufacturing of composite towers
Kayran, Altan (2014-06-01)
Numerical simulation of ice accretion and consequent power loss estimation in wind turbine blades
Özgen, Serkan; Berker, Ayşe Meriç; Çakmak, Ali (null; 2019-07-01)
The aim of this study is to simulate atmospheric ice accretion on wind turbine blades and to estimate power losses. A computational tool is developed that comprises six modules, one for estimating the local flow velocity and the angle of attack using the Blade Element Momentum Method (BEM), one for solving the flow field employing the Panel Method, one for computing the droplet trajectories with the Lagrangian approach, a module for calculating the convective heat transfer coefficients using the Integral Bo...
Aeroelastic Stability Evaluation of Bend Twist Coupled Composite Wind Turbine Blades Designed for Load Alleviation in Wind Turbine Systems
Farsadi, Touraj; Kayran, Altan (2016-01-04)
Wind turbine blades for turbines with large rotor diameter tend to be very flexible in order to remain weight and cost effective. Bending-twisting coupling induced in big composite wind turbine blades is one of the passive control mechanisms which is exploited to alleviate loads incurred due to the flexing of the blades. In the present study, aeroelastic stability characteristics of bend-twist coupled blades, designed for load alleviation in wind turbine systems, is investigated to check whether the bending...
Citation Formats
IEEE
ACM
APA
CHICAGO
MLA
BibTeX
T. Farsadi and A. Kayran, “Classical Aeroelastic Stability Analysis of Large Composite Wind Turbine Blades,” presented at the AIAA Science and Technology Forum and Exposition, 2016, Accessed: 00, 2021. [Online]. Available: http://arc.aiaa.org/series/6.scitech.