CIVENGC138
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CIVENG C138 - Flight Vehicle Structures and Aeroelasticity
Subject
CIVENG
Course Number
C138
Department
Course Level
Undergraduate
Course Title
Flight Vehicle Structures and Aeroelasticity
Course Description
This course introduces engineering students to the analysis and design of load-bearing components of flight structures, ranging from subsonic aircraft to rockets. Emphasis is placed on the quasi-static and dynamic analysis of structural components which are prevalent in aerospace engineering. Attention is also devoted to a comprehensive design roadmap of flight vehicle structures from the full system- to the individual component-level
Minimum Units
3
Maximum Units
3
Grading Basis
Default Letter Grade; P/NP Option
Method of Assessment
Written Exam
Instructors
Papadopoulos
Prerequisites
CIV ENG C30 / MEC ENG C85, and MEC ENG 104 or CIV ENG 126
Repeat Rules
Course is not repeatable for credit.
Credit Restriction Courses. Students will receive no credit for this course if following the course(s) have already been completed.
-
Credit Replacement Courses
-
Course Objectives
Student Learning Outcomes
Cross-Listed Course(s)
Formats
Lecture, Laboratory
Term
Fall and Spring
Weeks
15 weeks
Weeks
15
Lecture Hours
3
Lecture Hours Min
3
Lecture Hours Max
3
Laboratory Hours
1
Laboratory Hours Min
1
Laboratory Hours Max
1
Outside Work Hours
7
Outside Work Hours Min
7
Outside Work Hours Max
7