AE 114 - Aerospace Structures and Materials 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. Experimental stress measurements.

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

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