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This project provides a comprehensive framework for performing modal analysis and response evaluation of plane trusses. The project employs modal superposition techniques to analyze the dynamic behavior of structures subjected to shock (pulse) excitation.
This project provides a comprehensive framework for performing modal analysis and response evaluation of plane frames. The project employs modal superposition techniques to analyze the dynamic behavior of structures subjected to various types of excitations, with a particular focus on shock (pulse) excitation.
The vertical eigenfrequencies and mode shapes of a single-span suspension bridge are computed using the method by Luco et Turmo [1]. For the sake of completeness, the computed modal parameters are compared with those obtained using the method by Sigbjørnsson & Hjorth-Hansen [2] and Strømmen [3].
This project aims to study the dynamic behavior of a simplified model of an aircraft when rolling (steady state) when it is circulating stationary on the runway. The roughness of the track is the main exciting agent that will be considered in this project.