AVIA 31 - Aircraft Theory and Design

3 unit(s)
Aerodynamics and aeroelastics force. Load analysis of flight vehicles. Aircraft design optimization, material selection along with, safe-life, fail-safe and damage tolerance in design.

Lecture 2 hours/Lab 3 hours.

Prerequisite(s): PHYS 2A or PHYS 50; MATH 30 or MATH 71.
Grading: Letter Graded

High Impact Practice: Collaborative Assignments and Projects.

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