| Dersin Kodu | Dersin Adı | Dersin Türü | Yıl | Yarıyıl | AKTS | | MKM-23-101 | | Seçmeli | 1 | 2 | 0 |
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| Dersin Seviyesi |
| Yüksek Lisans |
| Dersin Amacı |
| The aim of this course is to provide the students with the ability to calculate basic cycle analysis by understanding the working principles of gas turbine engines. It also introduces the major components of each gas turbine engine. |
| Dersi Veren Öğretim Görevlisi/Görevlileri |
| Doç. Dr. Selçuk Ekici |
| Öğrenme Çıktıları |
| 1 | To have knowledge about turbojet engines. | | 2 | To have knowledge about turbofan engines. | | 3 | To have knowledge about turboprop engines. | | 4 | To have knowledge about turboshaft engines. | | 5 | To have knowledge about ramjet. | | 6 | To have knowledge about scramjet. |
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| Öğrenim Türü |
| Daytime Class |
| Dersin Ön Koşulu Olan Dersler |
| There is no prerequisite or co-requisite for this course. |
| Ders İçin Önerilen Diğer Hususlar |
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| Dersin İçeriği |
| Thermodynamics of aircraft/rocket/missile etc. propulsion and gas turbine engines, basic calculations and theoretical analysis and design of propulsion systems. |
| Haftalık Ayrıntılı Ders İçeriği |
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| 1 | Newton's laws and types of energy | | | | 2 | Connections between force, work, power, energy, speed and acceleration | | | | 3 | Turbojet engines and literature studies | | | | 4 | Turbofan engines and literature studies | | | | 5 | Turboshaft engines and literature studies | | | | 6 | Turboprop engines and literature studies | | | | 7 | To introduce the concepts of gross thrust, net thrust, conical nozzle thrust, thrust distribution, occurring thrust, thrust horsepower, equivalent shaft horsepower, specific fuel consumption | | | | 8 | To introduce static thrust, velocity-altitude-temperature, climate effects, engine efficiencies; by-pass ratio and pressure ratio, pressure, temperature and velocity of gas flow | | | | 9 | Major components: Turbines and Compressors introduction and thermodynamic analysis | | | | 10 | Major components: Combustion chamber introduction and thermodynamic analysis | | | | 11 | Chemical reactions in the combustion chamber and its relationship with propulsion | | | | 12 | Brayton Cycle | | | | 13 | First law analysis of gas turbine system | | | | 14 | First law analysis of gas turbine system | | |
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| Ders Kitabı / Malzemesi / Önerilen Kaynaklar |
| Advanced engineering thermodynamics
(Bejan, A. (2016). Advanced engineering thermodynamics. John Wiley & Sons.)
Aircraft propulsion and gas turbine engines
(El-Sayed, A. F. (2017). Aircraft propulsion and gas turbine engines. CRC press.)
Thermal design and optimization
(Bejan, A., Tsatsaronis, G., & Moran, M. J. (1995). Thermal design and optimization. John Wiley & Sons.)
Elements of Gas Turbine Propulsion
(Mattingly, J. D. (2006). Elements of propulsion: gas turbines and rockets. American Institute of Aeronautics and Astronautics.) |
| Planlanan Öğrenme Aktiviteleri ve Metodları |
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| Değerlendirme | |
| Midterm Examination | 1 | 100 | | TOPLAM | 100 | |
| Final Examination | 1 | 100 | | TOPLAM | 100 | | Term (or Year) Learning Activities | 40 | | End Of Term (or Year) Learning Activities | 60 | | TOPLAM | 100 |
| | Dersin Sunulduğu Dil | | Turkish | | Staj Durumu | |
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| İş Yükü Hesaplaması |
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| Midterm Examination | 1 | 1 | 1 |
| Final Examination | 1 | 1 | 1 |
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| Program ve Öğrenme Çıktıları İlişkisi |
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| * Katkı Düzeyi : 1 Çok düşük 2 Düşük 3 Orta 4 Yüksek 5 Çok yüksek |
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Iğdır University, Iğdır / TURKEY • Tel (pbx): +90 476
226 13 14 • e-mail: info@igdir.edu.tr
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