THERMAL TURBOMACHINERY
| Title | ΘΕΡΜΙΚΕΣ ΣΤΡΟΒΙΛΟΜΗΧΑΝΕΣ / THERMAL TURBOMACHINERY |
| Code | 315 |
| Faculty | Engineering |
| School | Mechanical Engineering |
| Cycle / Level | 1st / Undergraduate |
| Teaching Period | Winter |
| Coordinator | Anestis Kalfas |
| Common | Yes |
| Status | Active |
| Course ID | 20000346 |
Programme of Study: UPS of School of Mechanical Engineering
Registered students: 45
| Orientation | Attendance Type | Semester | Year | ECTS |
|---|---|---|---|---|
| Energy | Elective Course belonging to the selected specialization (Elective Specialization Course) | 9 | 5 | 5 |
| Design and Structures | Elective Course belonging to the selected specialization (Elective Specialization Course) | 9 | 5 | 5 |
| Academic Year | 2020 – 2021 |
| Class Period | Winter |
| Faculty Instructors |
|
| Weekly Hours | 5 |
| Class ID | 600170974
|
Mode of Delivery
- Face to face
Digital Course Content
- e-Study Guide https://qa.auth.gr/en/class/1/600170974
Erasmus
The course is also offered to exchange programme students.
Language of Instruction
- Greek (Instruction, Examination)
Prerequisites
General Prerequisites
Aerodynamics
Fluid Mechanics
Turbomachinery
Maths I, II, III
Learning Outcomes
The students will:
1. Learn and understand of the essential information regarding the performance and the characteristics of an aircraft
2. Learn and understand the aircraft design phases and how to proceed to the early phases of the aerodynamic design and performance calculation of a simple aircraft
3.
General Competences
- Apply knowledge in practice
- Retrieve, analyse and synthesise data and information, with the use of necessary technologies
- Adapt to new situations
- Make decisions
- Work autonomously
- Work in teams
- Work in an international context
- Generate new research ideas
- Design and manage projects
Course Content (Syllabus)
Conceptual, preliminary, detailed design. Specific aerodynamic data for aircraft wings. Aircraft performance (takeoff, climb, steady level flight, landing). Aircraft stability and control. Future designs. Aircraft design examples. Aerothermodynamics for reentry conditions.
Keywords
Design, performance, stability, control, reentry conditions, aircraft, aero engines, engine cycle, noise, pollutants
Educational Material Types
- Slide presentations
Use of Information and Communication Technologies
Use of ICT
- Use of ICT in Course Teaching
- Use of ICT in Laboratory Teaching
Description
Lectures
PowerPoint and video presentations
Communication:
Announcements, various information on the eclass platform
Personal communication by email
Course Organization
| Activities | Workload | ECTS | Individual | Teamwork | Erasmus |
|---|---|---|---|---|---|
| Lectures | 65 | 2.2 | ✓ | ||
| Fieldwork | 10 | 0.3 | ✓ | ||
| Reading Assigment | 52 | 1.7 | ✓ | ||
| Project | 20 | 0.7 | ✓ | ✓ | |
| Exams | 3 | 0.1 | |||
| Total | 150 | 5 |
Student Assessment
Student Assessment methods
- Written Exam with Short Answer Questions (Formative, Summative)
- Written Assignment (Formative, Summative)
- Oral Exams (Formative, Summative)
- Written Exam with Problem Solving (Formative, Summative)
Bibliography
Course Bibliography (Eudoxus)
Turbomachinery Flow Physics and Dynamic Performance [electronic resource]
Κωδικός Βιβλίου στον Εύδοξο: 171002
Συγγραφείς: Schobeiri, Meinhard.
ISBN: 9783540265917
Additional bibliography for study
Aircraft performance and design, J. D. Anderson Jr., McGraw-Hill
Aircraft Design: A Conceptual Approach, Daniel Raymer, AIAA Education Series
Last Update
22-10-2016
