FACULTY OF ENGINEERING
Department of Aerospace Engineering
SOCIAL MEDIA
AE 428 | Course Introduction and Application Information
| Course Name |
Hypersonic Systems
|
|
Code
|
Semester
|
Theory
(hour/week) |
Application/Lab
(hour/week) |
Local Credits
|
ECTS
|
|
AE 428
|
Fall/Spring
|
2
|
2
|
3
|
5
|
| Prerequisites |
None
|
|||||
| Course Language |
English
|
|||||
| Course Type |
Elective
|
|||||
| Course Level |
First Cycle
|
|||||
| Mode of Delivery | - | |||||
| Teaching Methods and Techniques of the Course | - | |||||
| Course Coordinator | ||||||
| Course Lecturer(s) | ||||||
| Assistant(s) | ||||||
| Course Objectives | The technologies necessary for the effective development of engines and structures for use in hypersonic systems are examined in this course. The course educates the highperformance systems necessary for ram/scramjet operation in all hypersonic regimes using a theoretical foundation, high temperature materials focusing on vehicle integration and compatibility with other propulsion cycles suggested for various hypersonic vehicle applications. |
| Learning Outcomes |
The students who succeeded in this course;
|
| Course Description | The course describes hypersonic flight vehicles and their performance,aerothermodynamics of hypersonic propulsion and hypersonic air breathing propulsion performance. In this course advanced high temperature materials, aerostructures and hypersonic aircraft concept design are discussed. |
|
|
Core Courses | |
| Major Area Courses |
X
|
|
| Supportive Courses | ||
| Media and Management Skills Courses | ||
| Transferable Skill Courses |
WEEKLY SUBJECTS AND RELATED PREPARATION STUDIES
| Week | Subjects | Related Preparation |
| 1 | Introduction to Hypersonic Propulsion | John, D. Anderson Jr.: Hypersonic and HighTemperature Gas Dynamics. AIAA, 2006. Chapter 1. |
| 2 | Review of Fundamental Principles | John, D. Anderson Jr.: Hypersonic and HighTemperature Gas Dynamics. AIAA, 2006. Chapter 2. |
| 3 | Aerothermodynamics | Bertin, J. J., Hypersonic Aerothermodynamics, AIAA Education Series, AIAA, Reston, VA, USA, 1994. Chapter 3. |
| 4 | Hypersonic Propulsion systems including: Inlets, Isolators, and Nozzles, Combustors and Fuels | Heiser, W.H. and Pratt, D. T.: Hypersonic Airbreathing Propulsion, 1994. ISBN: 1- 56347-035-7.Chapter 5. |
| 5 | Combined Cycle Propulsion: Technical Issues | Heiser, W.H. and Pratt, D. T.: Hypersonic Airbreathing Propulsion, 1994. ISBN: 1- 56347-035-7.Chapter 5. |
| 6 | Aeroacoustics, and flight vehicle force and moment characteristics | Viviani A., Pezzella G., Aerodynamic and Aerothermodynamic Analysis of Space Mission Vehicles. Springer, USA. 2015. Chapter 1. |
| 7 | Midterm | |
| 8 | High temperature materials, Structures and Thermal Management | Heiser, W.H. and Pratt, D. T.: Hypersonic Airbreathing Propulsion, 1994. ISBN: 1- 56347-035-7. Chapter 9. |
| 9 | Planetary entry, stage separation and atmospheric models | Viviani A., Pezzella G., Aerodynamic and Aerothermodynamic Analysis of Space Mission Vehicles. Springer, USA. 2015. Chapter 2. |
| 10 | CFD, Ground Testing, and Flight Demonstration | Viviani A., Pezzella G., Aerodynamic and Aerothermodynamic Analysis of Space Mission Vehicles. Springer, USA. 2015. Chapter 5. |
| 11 | Cooling/heat analysis and thermal protection systems | Griffin, M.D. and French, J.R. Space Vehicle Design, AIAA Education Series,. Washington D.C., 1991. ISBN: 1-56347-539-1. Chapter 6. |
| 12 | Hypersonic Vehicle Conceptual Design And Flight Programs | Griffin, M.D. and French, J.R. Space Vehicle Design, AIAA Education Series,. Washington D.C., 1991. ISBN: 1-56347-539-1 Chapter 6. |
| 13 | Hypersonic aircraft Conceptual Design | Heiser, W.H. and Pratt, D. T.: Hypersonic Airbreathing Propulsion, 1994. ISBN: 1- 56347-035-7. Chapter 3. |
| 14 | Student presentations | |
| 15 | Semester review | |
| 16 | Final |
| Course Notes/Textbooks | Heiser, W.H. and Pratt, D. T.: Hypersonic Airbreathing Propulsion, 1994. ISBN: 1-56347- 035-7. |
| Suggested Readings/Materials | John, D. Anderson Jr.: Hypersonic and High-Temperature Gas Dynamics. AIAA, 2006. ISBN 978-1-56347-780-5. Bertin, J. J., Hypersonic Aerothermodynamics, AIAA Education Series, AIAA, Reston, VA, USA, 1994. ISBN.978-1563470363 Viviani A., Pezzella G., Aerodynamic and Aerothermodynamic Analysis of Space Mission Vehicles. Springer, USA. 2015. ISBN: 978-3-319-13927-2. Griffin, M.D. and French, J.R. Space Vehicle Design, AIAA Education Series, Washington D.C., 1991. ISBN: 1-56347-539-1 |
EVALUATION SYSTEM
| Semester Activities | Number | Weigthing |
| Participation | ||
| Laboratory / Application |
1
|
10
|
| Field Work | ||
| Quizzes / Studio Critiques | ||
| Portfolio | ||
| Homework / Assignments | ||
| Presentation / Jury |
2
|
20
|
| Project | ||
| Seminar / Workshop | ||
| Oral Exams | ||
| Midterm |
1
|
30
|
| Final Exam |
1
|
40
|
| Total |
| Weighting of Semester Activities on the Final Grade |
4
|
60
|
| Weighting of End-of-Semester Activities on the Final Grade |
1
|
40
|
| Total |
ECTS / WORKLOAD TABLE
| Semester Activities | Number | Duration (Hours) | Workload |
|---|---|---|---|
| Theoretical Course Hours (Including exam week: 16 x total hours) |
16
|
2
|
32
|
| Laboratory / Application Hours (Including exam week: '.16.' x total hours) |
16
|
2
|
32
|
| Study Hours Out of Class |
14
|
3
|
42
|
| Field Work |
0
|
||
| Quizzes / Studio Critiques |
0
|
||
| Portfolio |
0
|
||
| Homework / Assignments |
0
|
||
| Presentation / Jury |
2
|
5
|
10
|
| Project |
0
|
||
| Seminar / Workshop |
0
|
||
| Oral Exam |
0
|
||
| Midterms |
1
|
17
|
17
|
| Final Exam |
1
|
17
|
17
|
| Total |
150
|
COURSE LEARNING OUTCOMES AND PROGRAM QUALIFICATIONS RELATIONSHIP
|
#
|
Program Competencies/Outcomes |
* Contribution Level
|
||||
|
1
|
2
|
3
|
4
|
5
|
||
| 1 | To have theoretical and practical knowledge that have been acquired in the area of Mathematics, Natural Sciences, and Aerospace Engineering. |
|||||
| 2 | To be able to assess, analyze and solve problems by using the scientific methods in the area of Aerospace Engineering. |
X | ||||
| 3 | To be able to design a complex system, process or product under realistic limitations and requirements by using modern design techniques. |
X | ||||
| 4 | To be able to develop, select and use novel tools and techniques required in the area of Aerospace Engineering. |
X | ||||
| 5 | To be able to design and conduct experiments, gather data, analyze and interpret results. |
X | ||||
| 6 | To be able to develop communication skills, ad working ability in multidisciplinary teams. |
|||||
| 7 | To be able to communicate effectively in verbal and written Turkish; writing and understanding reports, preparing design and production reports, making effective presentations, giving and receiving clear and understandable instructions. |
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| 8 | To have knowledge about global and social impact of engineering practices on health, environment, and safety; to have knowledge about contemporary issues as they pertain to engineering; to be aware of the legal ramifications of Aerospace Engineering solutions. |
|||||
| 9 | To be aware of professional and ethical responsibility; to have knowledge about standards utilized in engineering applications. |
|||||
| 10 | To have knowledge about industrial practices such as project management, risk management, and change management; to have awareness of entrepreneurship and innovation; to have knowledge about sustainable development. |
|||||
| 11 | To be able to collect data in the area of Aerospace Engineering, and to be able to communicate with colleagues in a foreign language (‘‘European Language Portfolio Global Scale’’, Level B1). |
|||||
| 12 | To be able to speak a second foreign language at a medium level of fluency efficiently. |
|||||
| 13 | To recognize the need for lifelong learning; to be able to access information, to be able to stay current with developments in science and technology; to be able to relate the knowledge accumulated throughout the human history to Aerospace Engineering. |
|||||
*1 Lowest, 2 Low, 3 Average, 4 High, 5 Highest
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