AE 251 - Structural Vibrations for Aerospace Applications

3 unit(s)
Introduces the analysis of vibrations of very flexible bodies encountered as elements of aircraft wings and space structures. Topics include: free and forced vibrations of single- and multi-degree of freedom systems, simplified analysis of vibrations induced by flutter, free and forced vibrations of wings in bending and torsion, signal processing techniques for time-varying signals, forced and ground vibration testing of aerospace components, finite element analysis for wings and space structures, spacecraft and aircraft dynamic design loads.

Prerequisite(s): BS in Aerospace Engineering or BS in Mechanical Engineering or instructor consent.
Grading: Letter Graded

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