Lecture 11 of 42Aerospace Propulsion
Cycle Analysis : Turbojet I
Dr. P.A. Ramakrishna · IIT Madras
Credits and licence
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- Aerospace Propulsion, IIT Madras (at NPTEL)
- Licence
- CC BY-NC-SA, as NPTEL states it. Non-commercial use only.
- Attribution
- NPTEL states: "Distributed under Creative Commons Attribution-ShareAlike / CC BY - NC - SA", beside a BY-NC-SA badge.
- Who can watch
- Tweens profiles and older. How courses are placed
All the lectures
- Introduction
- Air breathing Engines : Turbojet I
- Air breathing Engines : Turbojet II
- Air breathing Engines : Turboprop & Turbofan
- Air breathing Engines : Ramjet & Scramjet
- Non-air breathing Engines I
- Non-air breathing Engines II
- General Performance Parameters I
- General Performance Parameters II
- Cycle Analysis : Ramjet
- Cycle Analysis : Turbojet I
- Cycle Analysis : Turbojet II
- Cycle Analysis : Turbojet III
- Cycle Analysis : Turbojet IV
- Cycle Analysis : Turbojet V
- Cycle Analysis : Turbojet VI
- Cycle Analysis : Turbofan
- Rocket Nozzles : 1D Analysis I
- Rocket Nozzles : 1D Analysis II
- Rocket Nozzles : 1D Analysis III
- Rocket Nozzles : Real Effects I
- Rocket Nozzles : Real Effects II
- Rocket Nozzles : Thrust Vectoring
- Solid Rockets : Propellants
- Solid Rockets : Burn rate
- Solid Rockets : Performance
- Solid Rockets : Grain
- Solid Rockets : Ignition, Quenching
- Solid Rockets : Igniter, Depressurization
- Propellant Combustion : Combustion Modelling
- Liquid Rocket : Propellants
- Liquid Rocket : Nozzle Cooling I
- Liquid Rocket : Nozzle Cooling II
- Liquid Rocket : Nozzle Cooling III
- Liquid Rocket : Pressure fed system
- Liquid Rocket : Pump fed system
- Liquid Rocket : Pumps
- Liquid Rocket : Fuel Injection
- Hybrid Rocket : Basics
- Hybrid Rocket Performance
- Hybrid Rocket Combustion
- Chemical Equilibrium Analyser : SP 273