AVIA 31 - Aircraft Theory and Design

3 units
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.

Misc/Lab: Lecture 2 hours/Lab 3 hours.

Prerequisite(s): AVIA 2, PHYS 2A, MATH 71.
Pre/Corequisite(s): PHYS 2B
Grading: Graded

Class Schedule | Syllabus Information | University Bookstore