In this article, we
will be discussing how the coordinate transformation is carried out to
transform the element information i.e. element stiffness, element nodal displacements
and element nodal forces, in the local/element coordinate system oriented at an
angle to the global coordinate system.
This is a necessary step
to be perform before starting the element assembly process. We need to
check the orientation of local/element coordinate system xy-CS,
used for building the element model with reference to the global
coordinate system XY-CS. If the xy-CS
is aligned with the XY-CS, then, we can begin the assembly of
elements by constructing the element connectivity table as discussed in the previous article. Otherwise, it is essential to do coordinate transformation to align
the element local information to the global coordinate system before the
element assembly if the xy-CS is oriented at a certain angle
to
the XY-CS.
We need to transform
all information of an element model i.e. nodal displacements, nodal forces and
element stiffness matrix. In the below text, we discuss each of them one by
one.
Transformation of Element Nodal Displacements
Let consider a linear spring
element model with 2 nodes, as shown in Figure 1. Each node has 02 displacement
degrees of freedom, which are represented with blue colored vectors along the
element/local coordinate system xy-CS.
Please pay attention to the fact
that the xy-CS is NOT aligned to the global coordinate system XY-CS, and is
oriented at a certain angle. Therefore, we have to transform the blue colored
nodal displacements to red colored nodal displacements which are aligned to
XY-CS.
Figure
1. Transformation of element nodal displacement
Now, we discuss how to perform
this transformation of the element nodal displacements. Here is the geometrical
representation of the transformation between the components of nodal
displacements in xy-CS and XY-CS in Figure 2.
Figure 2. Geometrical representation of the nodal displacement transformation
In terms of mathematical equations, we can write the same geometrical representation of nodal displacement transformation as following in Figure 3.
Figure 3. Mathematical representation of the nodal displacement transformation
We prefer writing all nodal displacements in the following matrix form as a matter of convenience.
Where [
T] is the transformation matrix,
{u'} is the nodal displacement vector in the xy-CS oriented an angle, and
{u} is the nodal displacement vector in aligned with the XY-CS.
Transformation of Element Nodal Forces
In a similar fashion for the
nodal displacements, we can develop transformation relation for the nodal
forces as shown below in Figure 4.
Figure 4. Transformation of element nodal forces
The above information can be also present in the matrix form as below:
Where [T] is the same transformation matrix, {f'} is the nodal displacement vector in the xy-CS oriented an angle, and {f} is the nodal displacement vector in aligned with the XY-CS.
Transformation Matrix [T]
For conversion of nodal displacements and forces, we developed a transformation matrix [T] with entries of trigonometric sine and cosine ratios, shortly denoted by symbols l and m. This transformation matrix is a very special matrix because if we take its transpose or try to invert it, we get the same result. The matrix demonstrating such special property is called orthogonal matrix. Hence, the transformation matrix in our case is an orthogonal matrix as its transpose is equal to its inverse, as shown below.
The orthogonality of transformation matrix is very useful in numerical computation involving the matrix inversion. Whenever we need to inverse an orthogonal matrix, then, rather than taking its inverse we just take its transpose as inverting a matrix is a computationally expensive task as compare to taking its transpose which is merely the switching of its rows with columns. Please do remember that if a matrix is not an orthogonal matrix then we need takes its inverse as usual.
Transformation of Element Stiffness Matrix
So for we are able to develop the transformation relationships for the nodal displacement and load vectors using the transformation matrix [T], as shown below.
The remaining is the element stiffness matrix that also needs to be transformed from the xy-CS to the XY-CS. However, in this case use the previous transformation equations for the nodal displacements and forces, and manipulating them to derive the transformation relation for the element stiffness matrix as following.
Summary
Here is the summary of complete transformation relations for
the element information in xy-CS oriented at an angle to XY-CS.
Once all element information is fully transformed from -CS to -CS, then, we proceed to the assembly process by constructing the element connectivity table. For further details on the element assembly process, please
visit following article.
About the Author: Dr. Khazar
Hayat is a
professional engineer with almost 15+ year of experience in research, design,
analysis and development of products made of fiber reinforced plastics
composites (FRPCs). Currently, he is working as an Associate Professor at
Mechanical Engineering Department, The University of Lahore, Pakistan, can be
reaching by emailing at khazarhayat@gmail.com.
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