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
Structural dynamics analysis and passive control of wind turbine vibrations with tuned mass damper (TMD) technique
Date
2016-01-01
Author
Farsadi, Touraj
Kayran, Altan
Metadata
Show full item record
This work is licensed under a
Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
.
Item Usage Stats
172
views
0
downloads
Cite This
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.This paper investigates the use of a passive control device, tuned mass damper (TMD) for the control of vibrations of a simplified wind turbine. In the wind turbine model, tower and blades are modeled with continuous beam structure. Concentrated mass is considered as the nacelle. TMD system is placed at top of tower and attached to the nacelle. The coupled governing equation of motions and associated boundary conditions for the tower and the blades are obtained based on Euler-Bernoulli beam theory. In the present study, centrifugal force of blades due to rotation, lateral acceleration of the nacelle, self-weight and moment of inertia of nacelle and tower are considered in the analysis and aerodynamics loads are excluded in the analysis. Applying the Galerkin’s method with two admissible functions, the solution of the governing equations is obtained. In first part of the article, the coupled natural frequencies and mode shapes of wind turbine without TMD are calculated for various angular velocities of the blade. In the second part, it is shown how the TMD uniformly damps out the vibration of the selected coupled tower and blades mode.
Subject Keywords
Structural dynamics
URI
https://hdl.handle.net/11511/56287
DOI
https://doi.org/10.2514/6.2016-1481
Conference Name
57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
Collections
Department of Aerospace Engineering, Conference / Seminar
Suggestions
OpenMETU
Core
Implementation of ball-center spring analogy mesh deformation technique with CFD design optimization
Yang, Yosheph; Özgen, Serkan (2015-01-01)
© 2015, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.Mesh deformation technique plays an important role in several numerical simulations and applications including design optimization. This paper aims to implement the developed unstructured mesh deformation technique for CFD Design Optimization around 2-D Airfoils. During the optimization procedure, the newly deformed mesh is generated by using the updated Ball-Center Spring analogy mesh deformation technique. The compar...
Spin-axis tilt estimation for spinning spacecraft
Söken, Halil Ersin; Asamura, Kazushi; Nakamura, Yosuke; Takashima, Takeshi (2016-01-01)
© 2016 American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.The spin-axis tilt, which is also known as dynamic imbalance or coning error, is one of the most significant bias errors deteriorating the attitude determination accuracy for spinning spacecrafts. Although it is a common practical issue for spin spacecraft missions, estimation algorithms for the dynamic imbalance have not been studied and issued well. This paper proposes a simple algorithm for spin-axis tilt estimation....
A multi-fidelity, multi-disciplinary analysis and optimization framework for the design of morphing UAV wings
Ciarella, Andrea; Tsotskas, Christos; Hahn, Marco; Werter, Noud P. M.; De Breuker, Roeland; Beaverstock, Chris S.; Friswell, Michael I.; Yang, Yosheph; Özgen, Serkan; Antoniadis, Antonios; Tsoutsanis, Panagiotis; Drikakis, Dimitris (null; 2015-01-01)
© 2015 American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.A framework for the design and optimization of a morphing wing is presented. It allows the user to simplify the design process of a morphing UAV wing with a simple and effective interface with the possibility to easily switch between flight phases and morphing concepts. It consists of two main solvers: a high-fidelity CFD module for detailed RANS simulation and a fast low-fidelity module that solves the aeroelastic prob...
Aerodynamic optimization of wing-body configuration using discrete adjoint method
Yıldırım, Ahmet; Eyi, Sinan (2017-01-01)
© 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.The gradient based sensitivities required by design optimization are obtained by three different methods based on three dimensional Euler equations. Finite difference, Direct and Adjoint methods are used to compute objective sensitivities. A cell centered, upwind based finite volume method is implemented to discretize the Euler equations. The flow solution is obtained by preconditioned matrix-free Newton-GMRES algorith...
Aerodynamic parameter estimation of a supersonic air to air missile with rapid speed variation
Bayoglu, Tugba; Nalci, Mehmet Ozan; Kutay, Ali Türker (2016-01-01)
© 2016 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.Maneuver inputs designed for aircraft parameter identification are often applied during the aircraft flies close to a trimmed flight condition at an approximately constant Mach number. Since a fixed wing aircraft has control over its thrust and speed, various maneuver inputs can be applied to identify aerodynamic derivatives at discrete Mach numbers. On the contrary, most agile missile configurations do not have contr...
Citation Formats
IEEE
ACM
APA
CHICAGO
MLA
BibTeX
T. Farsadi and A. Kayran, “Structural dynamics analysis and passive control of wind turbine vibrations with tuned mass damper (TMD) technique,” presented at the 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, San Diego, California, USA, 2016, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/56287.