Dynamic analysis is required when inertia, time-dependent loading or impact changes the structural response. AeroMech evaluates whether resonance, amplification or local damage can govern the structural decision.
Dynamics require physical interpretation.
A calculated mode or transient response is not useful without understanding the corresponding deformation pattern, load path and sensitivity to mass and stiffness assumptions. AeroMech links numerical results to the physical structure.
Depending on the problem, the assessment may range from a simplified equivalent-static method to a nonlinear transient finite element analysis. The method and level of detail are selected to answer the engineering question.
