Research Article
Viscous and Aeroelastic Effects on Wind Turbine Blades. The VISCEL Project. Part II: Aeroelastic Stability Investigations
Article first published online: 1 JUL 2003
DOI: 10.1002/we.101
Copyright © 2003 John Wiley & Sons, Ltd.
Additional Information
How to Cite
Chaviaropoulos, P. K., Soerensen, N. N., Hansen, M. O. L., Nikolaou, I. G., Aggelis, K. A., Johansen, J., Gaunaa, M., Hambraus, T., von Geyr, H. Frhr., Hirsch, Ch., Shun, K., Voutsinas, S. G., Tzabiras, G., Perivolaris, Y. and Dyrmose, S. Z. (2003), Viscous and Aeroelastic Effects on Wind Turbine Blades. The VISCEL Project. Part II: Aeroelastic Stability Investigations. Wind Energ., 6: 387–403. doi: 10.1002/we.101
Publication History
- Issue published online: 21 NOV 2003
- Article first published online: 1 JUL 2003
- Manuscript Accepted: 4 APR 2003
- Manuscript Revised: 24 JAN 2003
- Manuscript Received: 4 DEC 2001
Funded by
- European Community (Joule III). Grant Number: JOR3-CT98-0208.
- Abstract
- References
- Cited By
Keywords:
- wind turbines;
- aeroelasticity;
- aeroelastic stability;
- Navier–Stokes solvers
Abstract
The recent introduction of ever larger wind turbines poses new challenges with regard to understanding the mechanisms of unsteady flow–structure interaction. An important aspect of the problem is the aeroelastic stability of the wind turbine blades, especially in the case of combined flap/lead–lag vibrations in the stall regime. Given the limited experimental information available in this field, the use of CFD techniques and state-of-the-art viscous flow solvers provides an invaluable alternative towards the identification of the underlying physics and the development and validation of sound engineering-type aeroelastic models. Navier–Stokes-based aeroelastic stability analysis of individual blade sections subjected to combined pitch/flap or flap/lead–lag motion has been attempted by the present consortium in the framework of the concluded VISCEL JOR3-CT98-0208 Joule III project. Copyright © 2003 John Wiley & Sons, Ltd.

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