Code |
Course Name |
Language |
Type |
MAK 4042 |
Gas Turbines |
Turkish |
Elective |
Local Credits |
ECTS |
Theoretical |
Tutorial |
Laboratory |
2.5 |
5.5 |
2 |
1 |
0 |
Course Prerequisites and Class Restriction |
Prerequisites |
TER 206 MIN DD or TER 206E MIN DD or MAK 4033 MIN DD or MAK 4033E MIN DD or MAK 212 MIN DD or MAK 212E MIN DD or MAK 226 MIN DD or MAK 226E MIN DD
|
Class Restriction |
4.Class |
Course Description |
Brayton cycle, turbo shafts. Flow in nozzles, Rayleigh and Fanno lines. Aircraft gas turbine engines: Thrust, parametric analysis,
pressure distribution in inlets and the diffusers, component efficiency. Turbomachinery: design of turbine and compressor blades.
Combustion systems. |
|