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

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