Advanced Principles of Propulsion
- main process of Gas turbine Design such as Design Parameters ، Constrains ، Objectives ، Analytical models optimization models
- Thermodynamic Analysis of Industrial Gas turbines Cycles
- Innovations in Industrial Gas turbine Cycles
- Thermodynamic Analysis of an Aero Gas turbine
- Intake System of an Aero Gas turbine
- Optimization of an Aero Gas Turbine Cycle
- Elements of Off Design Performance of Gas turbines
- Method of Calculation (Single Shaft).
Components Characteristic
Compatibility Equations
Simultaneous Equations
Running Line Definition
- Method of Calculation (Double Shaft)
- Load Classification
Constant Characteristic Load :
Generator type Loads
Traction Loads
- Part Load Performance
- Component Characteristic Estimate
- Part Load Remedy (Strategies)
- Off Design Performance of Single Spool Turbojet
Nozzle Characteristic
Component Characteristic and Compatibilities
Nozzle Characteristic
Simultaneous Equations برای بدست آوردن Running Line
Turbine and Nozzle in Series.
- Off Design Performance of Twin Spool Aero Gas turbines
- Transient Performance of Industrial Gas turbines
- Transient Performance of Aero Gas turbines