| Course Name |
Advanced Lightweight Structure
|
|
Code
|
Semester
|
Theory
(hour/week) |
Application/Lab
(hour/week) |
Local Credits
|
ECTS
|
|
AE 430
|
SPRING
|
2
|
2
|
3
|
5
|
| Prerequisites | None | |||||
| Course Language | English | |||||
| Course Type | ELECTIVE_COURSE | |||||
| Course Level | First Cycle | |||||
| Mode of Delivery | Face-to-face | |||||
| Teaching Methods and Techniques of the Course | - | |||||
| National Occupational Classification Code | - | |||||
| Course Coordinator |
|
|||||
| Course Lecturer(s) |
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|||||
| Assistant(s) | - | |||||
| Course Objectives | This course is for the design and analysis of lightweight structures with minimum weight for aerospace applications. This course is based on the student's ability to apply the principles of mathematics, material strength, and structural mechanics to design and analyze elements of lightweight aerostructures and space-related structures including launchers and space vehicles. | |||||||||||||||||||||||||||||||||||||||||||||||||||||
| Learning Outcomes |
The students who succeeded in this course;
|
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| Course Description | This course provides important tools for understanding the lightweight structure design process. The course consists of simulations accompanied by new topics and experiments, mainly related to composite and fiber modeling. In addition, this course includes various information of current interest in aeronautics and astronautics. | |||||||||||||||||||||||||||||||||||||||||||||||||||||
| Related Sustainable Development Goals |
-
|
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Core Courses |
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| Major Area Courses |
X
|
|
| Supportive Courses |
|
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| Media and Managment Skills Courses |
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| Transferable Skill Courses |
|
| Week | Subjects | Required Materials | Learning Outcome |
| 1 | Introduction: • History of lightweıght aerial structures • Aerospace systems design process • Structural design process | Niu, M.C.Y. Composite Airframe Structures, Technical Book Company, Los Angeles, 1996. Chapter 1. | LO1 |
| 2 | Loading: • Wing loading • Tail loading • Landing loading • Fuselage loading | Michael C. Y. Niu, Airframe Stress Analysis and Sizing, Conmilit Press Ltd, 2001. Chapter 2&3 | LO2 |
| 3 | Materials: • Physical and mechanical properties of lightweight materials • Application of composite materials and its selection process | Niu, M.C.Y. Composite Airframe Structures, Technical Book Company, Los Angeles, 1996. Chapter 2. | LO3 |
| 4 | Failure analysis: • Principles of stress analysis • Failure criterion for static loading • Fatigue accumulation damage in composite | Zagainov, G.I.; Lozino-Lozinski, G.E. Composite Materials in Aerospace Design, Chapman & Hall, London, 1996. Chapter 5. | LO3 |
| 5 | Structural instability: • Buckling of columns • Buckling of the reinforced sheet • Cylindrical shell buckling • Buckling of reinforced cylindrical shells | Michael C. Y. Niu, Airframe Stress Analysis and Sizing, Conmilit Press Ltd, 2001. Chapter 1. Chapter 7. | LO3 |
| 6 | Design and analysis of a typical aerial structure: • Wing design • Body design • Design of beams and ribs | Michael C. Y. Niu, Airframe Stress Analysis and Sizing, Conmilit Press Ltd, 2001. Chapter 6 and 8. | LO4 |
| 7 | Advanced composite manufacturıng | Mallick P. K., Fiber-Reinforced Composites Materials, Manufacturing and Design, CRC Press, 3rd Edition, 2008. Chapter 5. | LO3 |
| 8 | Midterm 1 | - | |
| 9 | Wave propagation in composite materials applicable to hypervelocity impact and integrity assessment | Datta S. K., Elastic waves in composite media and structures, CRC Press, Boca Raton, FL, 2009. Chapter 1 and 2. | LO3 |
| 10 | Advanced stress analysis methods usıng finite element, Multiscale Structural Modeling | Michael C. Y. Niu, Airframe Stress Analysis and Sizing, Conmilit Press Ltd, 2001. Chapter 5. | LO4 |
| 11 | Three textile composite for aero structures | Long A.C., Design and Manufacture of Textile Composites, wydaw. Woodhead Publishing, Cambridge 2005. Chapter 2. | LO3 |
| 12 | Performance analysis of preforms | Long A.C., Design and Manufacture of Textile Composites, wydaw. Woodhead Publishing, Cambridge 2005. Chapter 8. | LO4 |
| 13 | Non-destructive testing of composite for aero structures | Mallick P. K, Fiber-Reinforced Composites Materials, Manufacturing and Design, CRC Press, 3rd Edition, 2008. Chapter 6. | LO5 |
| 14 | Destructive testing of composite for aero structures | Mallick P. K., Fiber-Reinforced Composites Materials, Manufacturing and Design, CRC Press, 3rd Edition, 2008. Chapter 5. | LO5 |
| 15 | Semester review | Semester review | - |
| 16 | Final | Final | - |
| Course Notes/Textbooks | Niu M.C.Y Composite Airframe Structures Technical Book Company Los Angeles 1996. ISBN: 978-9627128069. |
| Suggested Readings/Materials |
Michael C. Y. Niu Airframe Stress Analysis and Sizing Conmilit Press Ltd 2001. ISBN: 978-9627128120 Zagainov G.I. Lozino-Lozinski G.E. Composite Materials in Aerospace Design Chapman & Hall London 1996 ISBN 978-94-010-4254-3 Mallick P. K. Fiber-Reinforced Composites Materials Manufacturing and Design CRC Press 3rd Edition 2008 Chapter 5. ISBN: 978-0-8493-4205-9 Datta S. K. Elastic waves in composite media and structures CRC Press Boca Raton FL 2009. ISBN:978-1420053388 Long A. C. Design and Manufacture of Textile Composites. Cambridge: Woodhead Publishing 2005. ISBN: 978-1855737440. |
| Semester Activities | Number | Weighting | LO1 | LO2 | LO3 | LO4 | LO5 |
| Laboratory / Application | 1 | 10 | X | X | X | X | X |
| Presentation / Jury | 1 | 10 | X | X | X | X | X |
| Midterm | 1 | 30 | X | X | X | ||
| Final Exam | 1 | 50 | 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 | 1 | 10 | 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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