AENG 510

Aircraft Structural Dynamics

Embry-Riddle Aeronautical University-Worldwide · UGRD · Fall 2026

1 section

Catalog description

Vibrations of deformable elastic structures using the assumed modes method. Analysis of a continuous system for specialized cases. Undamped and damped free and forced vibration of single-degree-of-freedom and multiple-degree-of-freedom system. Computer programming skills are necessary.

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Class #embry_riddle_aeronautical_worldw-0480Fall 2026UGRD3 credits

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Instructor: Staff

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