This work is considered to overview the applicability of modal dynamic method in seismic and aircraft crash analysis of NPP structures. Soil-structure interaction is taken into account; problem of 20%-limiting of modal composite damping is researched; results of different methods (Direct integration method, modal method, and upgraded modal method, when projected damping matrix is fully populated) are compared on test model and on real structure model. Simple test was solved theoretically and in ABAQUS, global damping matrices, acquired by modal and direct integration methods are compared. It is worth noting that both methods are approved for use in dynamic analysis of NPP structures by ASCE 4-98, but in most cases direct integration method gives more conservative results.
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