Contents:
Introduction & Development of Jet Aircraft Propulsion – How the Aircraft Jet Engines make Thrust – Jet Engine Basic Performance Parameters – Turbojet, Reheat Turbojet and Multi – spool Engines – Turbofan, Turbo-prop and Turboshaft engines-Ideal and Real Brayton cycles – Jet Engine Cycles for Aircraft propulsion – Cycle components and component performances – Analysis of engine real cycles – Thermodynamics of Compressors – Thermodynamics of Turbines – Axial Compressors : two dimensional analytical model – Cascade analysis; Loss and Blade performance estimation – Free Vortex theory; Single-Multi-stage characteristics – Elements of centrifugal compressor – Centrifugal Compressor characteristics: Surging, Choking – Axial flow turbines; Turbine Blade 2-D (cascade) analysis-Multi-staging: Axial Turbine; Turbine Cooling Technology

Radial Turbine Aerodynamics & Thermodynamics; Losses – Types of combustion chambers: mechanism & parameters – Pr. Loss, Combustion efficiency; Combustion intensity – Practical combustion system ; Stability, Fuel injection – Intakes for Powerplant: Transport / Military Aircraft-Subsonic, Transonic, Supersonic Intake Designs – Nozzle : fixed and variable geometry nozzles – C-D nozzle and their uses – Engine Off Design Operations – Aircraft Engine component matching: Dimensional analysis – Engine component matching and Sizing – Installed Performance of Engine – Use of Ramjets and Pulsejets in Aircraft propulsion – Thermodynamic Cycle & Performance Parameters – Flow in Diffusers, Combustors and Nozzles – Performanace and Design of Ramjet & Scramjet Engines – Future of Aircraft Propulsion

Other Resources

Course Curriculum

Introduction & Development of Jet Aircraft Propulsion Details
How the Aircraft Jet Engines make Thrust Details
Jet Engine Basic Performance Parameters Details
Turbojet, Reheat Turbojet and Multi-spool Engines Details
Turbofan, Turbo-prop and Turboshaft engines Details
Ideal and Real Brayton cycles Details
Jet Engine Cycles for Aircraft propulsion Details
Cycle components and component performances Details
Tute-1 Details
Analysis of engine real cycles Details
Tute-2 Details
Thermodynamics of Compressors Details
Thermodynamics of Turbines Details
Axial Compressors : two dimensional analytical model Details
Cascade analysis; Loss and Blade performance estimation Details
Free Vortex theory; Single-Multi-stage characteristics Details
Tutes — 3 Details
Elements of centrifugal compressor Details
Centrifugal Compressor characteristics: Surging, Choking Details
Axial flow turbines; Turbine Blade 2-D (cascade) analysis Details
Multi-staging: Axial Turbine; Turbine Cooling Technology Details
Radial Turbine Aerodynamics & Thermodynamics; Losses Details
Tutes — 4 Details
Types of combustion chambers: mechanism & parameters Details
Pr. Loss, Combustion efficiency; Combustion intensity Details
Practical combustion system ; Stability, Fuel injection Details
Intakes for Powerplant: Transport / Military Aircraft Details
Subsonic, Transonic, Supersonic Intake Designs Details
Nozzle : fixed and variable geometry nozzles Details
C-D nozzle and their uses Details
Tute-5 Details
Engine Off Design Operations Details
Aircraft Engine component matching: Dimensional analysis Details
Engine component matching and Sizing Details
Installed Performance of Engine Details
Tute-6 Details
Use of Ramjets and Pulsejets in Aircraft propulsion Details
Thermodynamic Cycle & Performance Parameters Details
Flow in Diffusers, Combustors and Nozzles Details
Performanace and Design of Ramjet & Scramjet Engines Details
Tute — 7 Details
Future of Aircraft Propulsion Details

This course is delivered by IIT Bombay , as part of NPTEL Free Courses sponsored by Govt of India.

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