Rotor Blade Aerodynamics Forces Modelling for Dynamic Analysis

Authors

  • Mohamed Abdalla Almheriegh Associate Professor, Department of civil Engineering, Faculty of Engineering - Tripoli University, P O Box 82677, Tripoli, Libya

Keywords:

ultimate loads on rotor blades, lift and drag forces, normal and tangential forces on blades, structural analysis of wind turbine blades

Abstract

In order to establish a rational method for structural analysis of wind turbine rotor with respect to failure in ultimate loading, either in strength or fatigue fashion. Two famous methods in predicting the complicated nature of the two main lift and drag forces acting ‘normal and tangential’ forces on the rotor blade are discussed and numerical solution ‘iteration’ using the coefficients involved in establishing these forces is presented and, therefore are readily introduced in the analysis stage typically done by dynamics analysis codes.

References

Freris L. L “Wind Energy Conversion Systems” Printice Hall 1996.

Walker F. J and Jenkins N “Wind Energy Technology” John Wiley & Sons UK 1997.

DET NORSKE VERITAS (DNV), Offshore Standard, DNV-OS-E301, Position Mooring, 2004, http://www.dnv.com, October 2004.

Det Norske Veritas “Guidelines for Design of Wind Turbines” second edition 2002, printed by Judsk Centraltrykkeri, Denmark ISBN 87-550-2870-5

Anders Ahlström “Simulating Dynamic Behaviour of Wind Power Structures” Licentiate Thesis Royal Institute of Technology, Department of Mechanics Stockholm2002. http://www2.mech.kth.se/~andersa/thesis/Licthesis.pdf, January 2003.

David M. Eggleston and Forrest S. Stoddard “Wind Turbine Engineering Design” 1987 Van Nostrand Inc. New York, ISBN 0-442-22195-9.

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Published

2021-10-09

How to Cite

Mohamed Abdalla Almheriegh. (2021). Rotor Blade Aerodynamics Forces Modelling for Dynamic Analysis. American Scientific Research Journal for Engineering, Technology, and Sciences, 82(1), 66–77. Retrieved from https://www.asrjetsjournal.org/index.php/American_Scientific_Journal/article/view/7072

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