| Course Name |
Aerospace Structures
|
|
Code
|
Semester
|
Theory
(hour/week) |
Application/Lab
(hour/week) |
Local Credits
|
ECTS
|
|
AE 426
|
FALL
|
2
|
2
|
3
|
5
|
| Prerequisites | To succesfully complete ME 211 (with a grade of at least DD) | |||||
| Course Language | English | |||||
| Course Type | Required (Core Course) | |||||
| Course Level | First Cycle | |||||
| Mode of Delivery | Face-to-face | |||||
| Teaching Methods and Techniques of the Course | - | |||||
| National Occupational Classification Code | - | |||||
| Course Coordinator |
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| Course Lecturer(s) |
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| Assistant(s) |
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| Course Objectives | This course aims to educate students on basic knowledge of structural mechanics and teach them to apply this fundamental knowledge in the aerospace structure problems particularly for analyzing the main structural elements of an aircraft and space vehicle structure. | |||||||||||||||||||||||||||||||||||||||||||||||||||||
| Learning Outcomes |
The students who succeeded in this course;
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| Course Description | The aeronautical structure course provides students with important tools to understand the analysis and design of aeronautical structures. It reviews the concepts of stress, strain, and elasticity equations. It covers the analysis of plane stress and plane strain problems with application to aeronautical structural elements including general bending and torsion of rods and beams and thin-walled structures and box girders. | |||||||||||||||||||||||||||||||||||||||||||||||||||||
| Related Sustainable Development Goals |
-
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Core Courses |
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| Major Area Courses |
X
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| Supportive Courses |
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| Media and Managment Skills Courses |
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| Transferable Skill Courses |
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| Week | Subjects | Required Materials | Learning Outcome |
| 1 | Introduction to flight vehicle structures | Michael C. Y. Niu, Airframe Stress Analysis and Sizing, Conmilit Press Ltd, 2001. Chapter 1. | LO1 |
| 2 | Familiarity with primary aerial structures and all forces acting on an aircraft | Megson, T.H.G.; An Introduction to Aircraft Structural Analysis, 4th Edition, ButterworthHeinemann, 2010. Chapter 2. | LO1 |
| 3 | Loading of aerospace structures, | Michael C. Y. Niu, Airframe Stress Analysis and Sizing, Conmilit Press Ltd, 2001. Chapter 3. | LO1 |
| 4 | Energy methods of structural analysis | Megson, T.H.G.; An Introduction to Aircraft Structural Analysis, 4th Edition, ButterworthHeinemann, 2010. Chapter 4. | LO2 |
| 5 | Two-dimensional elasticity | Megson, T.H.G.; An Introduction to Aircraft Structural Analysis, 4th Edition, ButterworthHeinemann, 2010. Chapter 8. | LO2 |
| 6 | Stress-strain laws | Michael C. Y. Niu, Airframe Stress Analysis and Sizing, Conmilit Press Ltd, 2001. Chapters 1 & 4. | LO2 |
| 7 | Yield and fatigue | Megson, T.H.G.; An Introduction to Aircraft Structural Analysis, 4th Edition, ButterworthHeinemann, 2010. Chapter 4. | LO3 |
| 8 | Midterm | - | |
| 9 | Bending of beams | Megson, T.H.G.; An Introduction to Aircraft Structural Analysis, 4th Edition, ButterworthHeinemann, 2010. Chapter 4. | LO3 |
| 10 | Torsion of beams, torsion of thin-walled cross sections | Megson, T.H.G.; An Introduction to Aircraft Structural Analysis, 4th Edition, ButterworthHeinemann, 2010. Chapter 4. | LO3 |
| 11 | Combined bending torsion of thin-walled | Megson, T.H.G.; An Introduction to Aircraft Structural Analysis, 4th Edition, ButterworthHeinemann, 2010. Chapter 4. | LO4 |
| 12 | Stiffened composite structures used in aerospace vehicles | Megson, T.H.G.; An Introduction to Aircraft Structural Analysis, 4th Edition, ButterworthHeinemann, 2010. Chapter 4. | LO5 |
| 13 | Elements of plate theory, buckling of columns | Megson, T.H.G.; An Introduction to Aircraft Structural Analysis, 4th Edition, ButterworthHeinemann, 2010. Chapter 4. | LO5 |
| 14 | Summary on designing aerospace structures and their connections | Megson, T.H.G.; An Introduction to Aircraft Structural Analysis, 4th Edition, ButterworthHeinemann, 2010. Chapter 4. | LO5 |
| 15 | Semester review | Semester review | - |
| 16 | Final | Final | - |
| Course Notes/Textbooks | Megson T.H.G. An Introduction to Aircraft Structural Analysis 4th Edition Butterworth Heinemann 2010. ISBN: 978-0-08-098201-4. |
| Suggested Readings/Materials | Michael C. Y. Niu Airframe Stress Analysis and Sizing Conmilit Press Ltd 2001. ISBN 962- 7128-08-2. |
| Semester Activities | Number | Weighting | LO1 | LO2 | LO3 | LO4 | LO5 |
| Laboratory / Application | 1 | 10 | X | X | X | X | X |
| Presentation / Jury | 1 | 20 | X | X | X | X | X |
| Midterm | 1 | 30 | X | X | X | X | |
| Final Exam | 1 | 40 | X | X | X | X | X |
| Total | 4 | 100 |
| Semester Activities | Number | Duration (Hours) | Workload |
|---|---|---|---|
| Participation | - | - | - |
| Theoretical Course Hours | 16 | 2 | 32 |
| Laboratory / Application Hours | 16 | 2 | 32 |
| Study Hours Out of Class | 14 | 3 | 42 |
| Field Work | - | - | - |
| Quizzes / Studio Critiques | - | - | - |
| Portfolio | - | - | - |
| Homework / Assignments | - | - | - |
| Presentation / Jury | 2 | 5 | 10 |
| Project | - | - | - |
| Seminar / Workshop | - | - | - |
| Oral Exams | - | - | - |
| Midterms | 1 | 17 | 17 |
| Final Exam | 1 | 17 | 17 |
| Total | 150 |
| # | PC Sub | Program Competencies/Outcomes | * Contribution Level | ||||
| 1 | 2 | 3 | 4 | 5 | |||
| No program competency data found. | |||||||
*1 Lowest, 2 Low, 3 Average, 4 High, 5 Highest
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