AVIA 31 - Aircraft Theory and Design
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): AVIA 2, PHYS 2A,MATH 71 or MATH 71X.
Pre/Corequisite(s): PHYS 2B.
Grading: Letter Graded
Class Schedule | Syllabus Information | University Bookstore
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