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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

AENG 510-WW
Campus
Worldwide
College of Aeronautics (WAERO)
AENG
510
Aircraft Structural Dynamics
3
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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Written assignments must be formatted in accordance with the current edition of the Publication Manual of the American Psychological Association (APA) unless otherwise instructed in individual assignments.

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