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AENG 510 : Aircraft Structural Dynamics

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Last approved: Tue, 09 Aug 2016 17:50:58 GMT

Last edit: Tue, 09 Aug 2016 17:50:57 GMT

College of Aeronautics (WAERO)
Aircraft Structural Dynamics
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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ActivityPercent of Grade
Input Grading Item100

Undergraduate Grade Scale

90 - 100% A
80 - 89% B
70 - 79% C
60 - 69% D
0 - 60% F

Graduate Grade Scale

90 - 100% A
80 - 89% B
70 - 79% C
0 - 69% F
Key: 482