ME60098: Gas Turbines And Jet Propulsion
Jump to navigation
Jump to search
| ME60098 | |||||||||||||||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Course name | Gas Turbines And Jet Propulsion | ||||||||||||||||||||||||
| Offered by | Mechanical Engineering | ||||||||||||||||||||||||
| Credits | 4 | ||||||||||||||||||||||||
| L-T-P | 3-1-0 | ||||||||||||||||||||||||
| Previous Year Grade Distribution | |||||||||||||||||||||||||
| |||||||||||||||||||||||||
| Semester | Spring | ||||||||||||||||||||||||
Syllabus
Syllabus mentioned in ERP
Thermodynamic cycle analysis of gas turbines; open and closed cycles. Axial flow turbines; blade diagrams and design of blading, performance characteristics. Centrifugal and axial flow compressors, blowers and fans. Theory and design of impellers and blading. Matching of turbines and compressors. Fuels and combustion, effect of combustion chamber design and exhaust on performance. Basic principles and methods of heat recovery. Thermodynamic cycle analysis and efficiencies of propulsive devices. Thrust equation, classification and comparison of ram jets, turbojets, pulse jets and rockets. Performance of turbo-prop, turbo-jet and turbo-fan engines. Augmentation of thrust.