AEROENGC184
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Flight Vehicle Structures and Aeroelasticity
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
3
Maximum
3
Grading Basis
Default Letter Grade; P/NP Option
Method of Assessment
Written Exam
Instructors
Papadopoulos
American Cultures Requirement
No
Reading and Composition Requirement
None of the Reading and Composition Requirement
Prerequisite
Complete ANY of the following Courses:
Complete ANY of the following Courses:
Repeat Rules
Course is not repeatable for credit.
Credit Restriction Courses. Students will receive no credit for this course if the following the course(s) have already been completed.
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Credit Replacement Courses. Upon passing, students can use the following course(s) to replace a deficient grade for this course.
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Course Objectives
Student Learning Outcomes
Cross-Listed Course(s)
Formats
Lecture, Laboratory
Term
Fall and Spring
Duration (in weeks)
15
Minimum Hours
3
Maximum Hours
3
Minimum Hours
1
Maximum Hours
1
Outside Work Hours Min
7
Maximum Hours
7