This study presents a transient dynamic analysis of a 3D-printed composite cantilever beam fabricated from short carbon fibre-reinforced polyamide (CF-PA-12). Particular attention is given to acceleration response, vibration damping, and energy dissipation, which govern the transient behaviour and dynamic stability of lightweight composite structures under impulsive loading. The research combines experimental modal analysis (EMA) and transient impact testing with numerical simulations based on classical laminated plate theory (CLPT). A finite element model was developed in Simulia/Abaqus and used within a modal-superposition-based transient framework incorporating experimentally identified damping ratios and measured impact forces. The proposed approach enables realistic prediction of vibration decay and time-dependent acceleration response. Good agreement between experimental and numerical results confirms the capability of the method to reproduce the dynamic behaviour of additively manufactured composite beams subjected to impact excitation.
Wesołowski et al. (Thu,) studied this question.