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AVIA 031

Aircraft Theory and Design

Description
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. Prerequisite: AVIA 2, PHYS 2A, MATH 71. Pre/Co-requisite: PHYS 2B Misc/Lab: Lecture 2 hours/Lab 3 hours.

Grading
Normal Grade Rules

Units
3