AE6220: Rotorcraft Structural Dynamics and Aeroelasticity

3 Credits

Elementary blade dynamics, flap-lag dynamics, ground resonance, structural dynamics of rotating beams, nonlinear elastic blade analysis, harmonic balance and trim, Floquet theory.

Requisites

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GPA: 3.60Most Common: A (57.8%)

This total includes data from semesters with unknown instructors

64 students
WVFDCBA


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