The idea behind the modal superposition transient stress analysis is to sum factored mode shapes (eigenvectors) from a modal analysis to calculate the structure's response under dynamic loading.
Then,
{u}=[Phi]{Modal Coordinates Vector}
where, [Phi] is the modal matrix (consisting of mode shapes) and {u} is the displacement vector.
However, this idea is used to calculate stresses based on the following expression:
{Sigma}=[Modal Stress Matrix]{Modal Coordinates Vector}
Now the question is, how modal stress matrix is defined and what's its physical interpretation?
Thanks