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Research Papers

A Continuum Based Three-Dimensional Modeling of Wind Turbine Blades

[+] Author and Article Information
Ahmed H. Bayoumy

Graduate Student
Mechanical Design & Production,
Engineering Department,
Faculty of Engineering,
Cairo University,
Giza 12613, Egypt
e-mail: a.hamdy85@ymail.com

Ayman A. Nada

Assistant Professor
Mechanical Engineering Department,
Benha Institute of Technology,
Benha University,
Benha 13512, Egypt
e-mail: arobust@tedata.net.eg

Said M. Megahed

Professor
Mechanical Design & Production,
Engineering Department,
Faculty of Engineering,
Cairo University,
Giza 12613, Egypt
e-mail: smegahed@cu.edu.eg

1Corresponding author.

2Present address: College of Engineering, Jazan University, Jazan P.O.706, KSA.

Contributed by the Design Engineering Division of ASME for publication in the Journal of Computational and Nonlinear Dynamics. Manuscript received December 5, 2011; final manuscript received August 18, 2012; published online October 30, 2012. Assoc. Editor: Khaled E. Zaazaa.

J. Comput. Nonlinear Dynam 8(3), 031004 (Oct 30, 2012) (14 pages) Paper No: CND-11-1237; doi: 10.1115/1.4007798 History: Received December 05, 2011; Revised August 18, 2012

Accurate modeling of large wind turbine blades is an extremely challenging problem. This is due to their tremendous geometric complexity and the turbulent and unpredictable conditions in which they operate. In this paper, a continuum based three dimensional finite element model of an elastic wind turbine blade is derived using the absolute nodal coordinates formulation (ANCF). This formulation is very suitable for modeling of large-deformation, large-rotation structures like wind turbine blades. An efficient model of six thin plate elements is proposed for such blades with non-uniform, and twisted nature. Furthermore, a mapping procedure to construct the ANCF model of NACA (National Advisory Committee for Aeronautics) wind turbine blades airfoils is established to mesh the geometry of a real turbine blade. The complex shape of such blades is approximated using an absolute nodal coordinate thin plate element, to take the blades tapering and twist into account. Three numerical examples are presented to show the transient response of the wind turbine blades due to gravitational/aerodynamics forces. The simulation results are compared with those obtained using ANSYS code with a good agreement.

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References

Figures

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Fig. 1

Airfoil shape parameters

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Fig. 3

Four nodes plate element

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Fig. 5

Constructing airfoil using ANCF (2 elements)

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Fig. 6

NACA and ANCF airfoils (2 elements)

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Fig. 7

Constructing airfoil using ANCF (6 elements)

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Fig. 8

ANCF models of NACA airfoils, red lines represent NACA code profile

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Fig. 9

Nonuniform wind turbine blade

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Fig. 10

WTB NACA 4412, α = 5 (deg)

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Fig. 11

WTB NACA 8612, α = 8 (deg)

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Fig. 12

Twisted wind turbine blade

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Fig. 13

WTB: twisted NACA 4412, β = 30 (deg)

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Fig. 14

WTB: front view: twisted NACA 4412, β = 30 (deg)

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Fig. 15

WTB: twisted NACA 8612, β = 30 (deg)

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Fig. 16

WTB: front view: twisted NACA 8612, β = 30 (deg)

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Fig. 17

Aerodynamic forces

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Fig. 18

FEM blade model with ANSYS (nontapered blade)

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Fig. 19

Transverse deflection of tip edge point

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Fig. 20

FEM blade model with ANSYS (tapered blade)

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Fig. 21

Transverse deflection of tip edge point

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Fig. 22

ANSYS meshing domains of blade-wall and fluid

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Fig. 23

Transient response of aerodynamic forces with ANSYS

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Fig. 24

Comparison of aerodynamics responses

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Fig. 25

WTB model with multisections along the span length

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Fig. 26

Comparison of different models along the span length

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