AE 114 - Aerospace Structural Analysis II

3 unit(s)
Aircraft, missile, spacecraft structural design and analysis. Static, elastic and stress analysis of structures. Structural materials. Deflection analysis of structural systems. Conventional, stiffened, sandwich and composite structures. Structural dynamics. Thermal effects.

Prerequisite(s): C or better in AE 112 or graduate standing.
Grading: Letter Graded

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