Prof. Dr. Muhsin Kılıç mkilic@uludag.edu.tr Adres: Uludağ Üniversitesi Mühendislik-Mimarlık Fakültesi Ali Durmaz Makine Mühendisliği Binası DM:220 16059 Görükle/BURSA Tel: 0224 294 1953
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Website:
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Objective of the Course:
Mechanical engineering students with the gas and steam turbines, compressors, such as energy production, particularly the most widely used for various purposes, including the principles of thermal turbo machines, to teach the fundamentals of design and calculation methods in designing
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Contribution of the Course to Professional Development
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Learning Outcomes:
1
Turbomachinery, general definitions, classifications, will be familiar with basic dimensions;
2
Thermal turbo machines, classes, and knows the area of use
;
3
For subsonic and supersonic flows, like nozzle and diffuser design elements can made ;
4
For radial-flow compressor calculation and design methods can be learnt;
5
For radial-flow turbine calculation and design methods can be learnt;
6
For Axial-flow compressor calculation and design methods can be learnt;
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For Axial-flow turbine calculation and design methods can be learnt;
8
Have a basic knowledge on the use of thermal turbo machines at heat and power plants. ;
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Course Content:
Week
Theoretical
Practical
1
Introduction of the course, given the content, giving students the resources and the measurement method. Turbo Machines Introduction, Dimensional Analysis, Similarity.
2
Introduction of thermal turbo machines in the lab. Thermodynamics and Fluid Mechanics required for thermal turbo machines reminder of basics. I. Thermodynamics And II. Laws. Theorem of linear momentum, angular momentum theorem, the Euler equation
3
that the flow nozzle and diffusers, stagnation properties, the speed of sound, subsonic and supersonic flow speeds. Convergent, convergent-divergent nozzle and diffusers. Nozzle and diffuser efficiencies. Actual nozzle and diffuser efficiencies. Problem solving and application.
4
The compressor and turbine efficiencies. Problems solving
5
Two-dimensional flow for kaskats. Concepts, force analysis, minor losses. Wing design
6
Two-dimensional flow for kaskats. Concepts, force analysis, minor losses. Wing design. Example problems solving.
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Repeating courses and midterm exam
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Radial-flow turbines
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Radial-flow compressor
10
Example problems solving about radial-flow turbines and compresor
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Axial-flow turbine
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Axial-flow compressor
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Example problems solving about axial-flow turbines and compresor
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Performance evaluation of thermic turbo-machinery design and the non-use of design
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Textbooks, References and/or Other Materials:
Turbomakinelerde Akış: Turbomakinelerin Termodinamiği ve Akışkanlar Mekaniği, E. Öztürk, Birsen Yayınevi, 1997, İstanbul. Örneklerle Termik Turbo Makinaların Prensipleri, N. Kayansayan, DEÜ, 1986, İzmir. Fluid Mechanics and Thermodynamics of Turbomachinery, 3rd Ed., S.L. Dixon , Pergoman Press Ltd., 1978, Oxford
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Assesment
TERM LEARNING ACTIVITIES
NUMBER
PERCENT
Midterm Exam
1
30
Quiz
0
0
Homeworks, Performances
1
20
Final Exam
1
50
Total
3
100
Contribution of Term (Year) Learning Activities to Success Grade
50
Contribution of Final Exam to Success Grade
50
Total
100
Measurement and Evaluation Techniques Used in the Course
Information
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ECTS / WORK LOAD TABLE
Activites
NUMBER
TIME [Hour]
Total WorkLoad [Hour]
Theoretical
14
3
42
Practicals/Labs
0
0
0
Self Study and Preparation
14
3
42
Homeworks, Performances
1
45
45
Projects
0
0
0
Field Studies
0
0
0
Midtermexams
1
2
2
Others
1
62
62
Final Exams
1
2
2
Total WorkLoad
195
Total workload/ 30 hr
6,5
ECTS Credit of the Course
6,5
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CONTRIBUTION OF LEARNING OUTCOMES TO PROGRAMME QUALIFICATIONS
