Any matrix can be decomposed into a sum of symmetric and antisymmetric matrices, but can be decomposed into a product of two matrices (one symmetric and one orthogonal)
(1)
and
are called the Right Stretch Tensor and Left Stretch Tensor due to their respective positions (relative to
) in eq. 1.
(symmetric)
(symmetric)
(orthogonal)
A proof of the orthogonality of is given in Appendix A.3.
(2)
(3)
is a rigid body rotation, while
or
each stretch and rotate (they each contain both normal and shear deformations, typically)
and
have the same eigenvalues. Eigenvalues do not have an “order,” per se, but since
and
typically have different eigenvectors, one should be cautious when assuming equivalency of eigenvalues. In the principal directions of
or
,
or
contains no shear deformation (see Fig). We’ll look at actual stresses, later.
To find the principal directions of and
, we must solve the eigenvalue problem:
(pictured)
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e.x. Polar Decomposition
The deformed equilibrium configuration of a body defined by the deformation mapping:
,
,
Determine:
a) and
b) Eigenvalues and eigenvectors of
c) and
d)
e)
a) =
note:
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b) ;
;
;
i.e. for ,
Choose arbitrary ; solve for
from either equation ; normalize:
c)
(symmetric)
where
It’s important to keep in mind that ,
, and
have the same eigenvectors and that these eigenvectors (and any other strain direction or magnitude) are generally dependent on the particular point in space of interest (e.g.
,
,
). For this simple example,
is independent of
,
, and
(i.e. the deformation is the same everywhere in the body – a “homogenous” deformation), but this would generally not be the case.
The eigenvalues occur in the direction of the eigenvectors, thus, ;
;
. It makes sense that if we only know the eigenvectors and want to undo this transformation to bring us back to
, then we need a transformation matrix that involves
. We can see that
is the opposite of the usual
, and without going through the rigorous derivation of why
,
,
, it at least makes some sense intuitively.
d) (orthogonal ;
e)