Fundamentals Of Propulsion
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Fundamentals Of Propulsion Syllabus — Unit-wise Content
The official GTU curriculum for Fundamentals Of Propulsion (subject code 3350104) as prescribed for CIVIL · Semester 5 divides the course into 5 units, covering 39 listed topics. The unit-wise breakdown below is read from the GTU syllabus document for this subject code, so you can check what the course actually covers before deciding which papers to attempt.
Download the official syllabus PDF (3350104)Unit 1 INTRODUCTION Basic of thermodynamics Newton laws of motion To study about thrust & its factor To study about
- 1.1. Reviews of thermodynamic principles
- 1.2. Newton’s laws of motion
- 1.3. Modes of heat transfer
- 1.5. Factors effecting the thrust
- 1.6. Efficiency FUNDAMENTALS OF PROPULSION Course Code: 3350104 GTU/ NITTTR Bhopal/16 Gujarat State 2 governing cycle of gas turbine engines
- 1.7. Brayton cycle
- 1.8. Governing equation
Unit 2 AIRCRAFT ENGINES To Study propulsion history To study about IC engines To study about various gas turbine
- 2.1. Classification propulsion system
- 2.2. Internal combustion engines
- 2.3. Gas turbine engine
- 2.4. Ramjet engine
- 2.5. Rocket engine
- 2.6. Turbojet engine
- 2.7. Turboprop engine
- 2.8. Turbofan engines
- 2.9. Thrust augmentation
- 2.10. Diffusion mass transfer
- 2.11. Accessory section
- 2.12. Auxiliary power unit
Unit 3 INLET, COMPRESSOR & DIFFUSER To study about inlet of engine. To study about compressor & its types. To about diffuser.
- 3.2. Compressor a. Types of compressor b.Efficiency of compressor c. Compressor design parameters d.Bleed air utilization e. Dual compressor theory f. Variable inlet vane & stator
Unit 4 COMBUSTION CHAMBER & NOZZLE To study about combustion chamber To study about combustion characteristic To study about fuel
- 4.1. Combustion chamber
- 4.2. Factors affecting combustion chamber design, process & performance
- 4.3. Requirements of combustion chamber
- 4.4. Combustion chamber process
- 4.5. Types of combustion chamber
- 4.6. Combustion chamber stability & instability
- 4.7. Fuel injection system
- 4.9. Types of nozzle
- 4.10. Throat condition for supersonic nozzle
- 4.11. Nozzle efficiency
- 4.12. Under expanding & over- expanding nozzle
- 4.13. Variable area nozzle
- 4.14. Thrust reversal
Unit 5 TURBINES To study principle turbine. To study about compounding of turbines.
- 5.1. Operating principle of impulse turbines
- 5.2. Operating principle of Reaction turbines
- 5.3. Velocity Triangle
- 5.4. Blades FUNDAMENTALS OF PROPULSION Course Code: 3350104 GTU/ NITTTR Bhopal/16 Gujarat State 3
- 5.5. Velocity & Pressure compounding of multistage impulse turbine
- 5.6. Degree of Reaction
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