wind turbine blade design using fem
DESCRIPTION
Wind turbine blade design using FEM. Afolabi Akingbe Wei Cheng Wenyu Zhou. Outline. Basics of wind turbine blade Blade element theory Membrane & plate bending model Shell element in FEM ANSYS model. How wind turbine blades work. Essential blade concepts. chord. Twist angle. - PowerPoint PPT PresentationTRANSCRIPT
Wind turbine blade design using FEMAFOLABI AKINGBE
WEI CHENG
WENYU ZHOU
OutlineBasics of wind turbine bladeBlade element theoryMembrane & plate bending modelShell element in FEMANSYS model
How wind turbine blades work
Essential blade conceptschord
Twist angle
Blade element theory
Membrane & plate bending3D structures under arbitrary loads
Split element into two types for different calculations
Membrane element for in-plane loads
Plate bending elements for transverse loads and bending
FEM triangular blade model
Membrane element analysis
Assume linear displacements
◦ are 2x2 matrices
Membrane element analysis
Bending element analysis
Tranverse displacements and rotations are taken as degrees of freedom.◦
◦ are 4x4 matrices
Bending element analysis
FEM for shell analysisA combination of a plate bending and membrane element
The DOF of a plate and plane stress finite element in a local element-aligned coordinate system are considered
Shell element
(a) Plane deformation (b) bending deformation
The finite element solution
Displacement model The displacement model for the flat shell is expressed as
Ni is the bilinear shape functions associated to node i,
and
Strain and curvature The membrane εm and curvature κ are defined as
Transverse shear strain is
Approximation of strain field
The membrane deformation, the approximation of the strain field is
Discrete curvature field The discrete curvature field is
Approximation of shear strain
The approximation of shear strain is written as
Linear system Combining simultaneously membrane and bending actions, a linear system for the vector of nodal unknowns q can be written
where ke is the stiffness matrix composed of membrane and plate stiffness element matrices
Load vector The load vector at each node i is of the form
fie = [Fxi Fyi Fzi Mxi Myi Mzi ]T
Element stiffness matrix The element stiffness matrix at each node i
ANSYS Modeling
• Angular velocity
• Surface pressure
Deformation & stress contours
More stress at the blade root
Thicker material closer to root to endure high loads
(Displacement contour)
(Stress contour)
Composite Can use commercial code like ANSYS to quickly change material properties and mesh sizing.