Learn · Jet Aircraft Propulsion
Lecture 35 of 42Jet Aircraft Propulsion
L35-Installed Performance of Engine
Prof. Bhaskar Roy and Prof. A M Pradeep · IIT Bombay
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- Jet Aircraft Propulsion, IIT Bombay (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.
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- Teens profiles and older. How courses are placed
All the lectures
- L1-Introduction & Development of Jet Aircraft Propulsion
- L2-How the Aircraft Jet Engines make Thrust
- L3-Jet Engine Basic Performance Parameters
- L4-Turbojet, Reheat Turbojet and Multi-spool Engines
- L5-Turbofan, Turbo-prop and Turboshaft engines
- L6-Ideal and Real Brayton cycles
- L7-Jet Engine Cycles for Aircraft propulsion
- L8-Cycle components and component performances
- L9-Tute-1
- L10-Analysis of engine real cycles
- L11-Tute-2
- L12-Thermodynamics of Compressors
- L13-Thermodynamics of Turbines
- L14-Axial Compressors : two dimensional analytical model
- L15-Cascade analysis; Loss and Blade performance estimation
- L16-Free Vortex theory; Single-Multi-stage characteristics
- L17-Tutes - 3
- L18-Elements of centrifugal compressor
- L19-Centrifugal Compressor characteristics: Surging, Choking
- L20-Axial flow turbines; Turbine Blade 2-D (cascade) analysis
- L21-Multi-staging: Axial Turbine; Turbine Cooling Technology
- L22-Radial Turbine Aerodynamics & Thermodynamics; Losses
- L23-Tutes - 4
- L24-Types of combustion chambers: mechanism & parameters
- L25-Pr. Loss, Combustion efficiency; Combustion intensity
- L26-Practical combustion system ; Stability, Fuel injection
- L27-Intakes for Powerplant: Transport / Military Aircraft
- L28-Subsonic, Transonic, Supersonic Intake Designs
- L29-Nozzle : fixed and variable geometry nozzles
- L30-C-D nozzle and their uses
- L31-Tute-5
- L32-Engine Off Design Operations
- L33-Aircraft Engine component matching: Dimensional analysis
- L34-Engine component matching and Sizing
- L35-Installed Performance of Engine
- L36-Tute-6
- L37-Use of Ramjets and Pulsejets in Aircraft propulsion
- L38-Thermodynamic Cycle & Performance Parameters
- L39-Flow in Diffusers, Combustors and Nozzles
- L40-Performanace and Design of Ramjet & Scramjet Engines
- L41-Tute - 7
- L42-Future of Aircraft Propulsion