Jet Aircraft Propulsion NPTEL
Online Free Online Course by
World Mentoring Academy
Online
/ Free Online Course
Details
Description: Introduction to Aircraft Jet Propulsion. Jet Engine Cycles : Thermodynamic Analysis of real cycles. Compressors and Turbines. Combustion Systems. Intakes and Propelling Nozzles. Aircraft Engine Installed Performance, Sizing &
Matching. Ramjets, Scramjets and Pulsejets.
Resources: OpenCourseware from NPTEL (India), Sheridan College, MIT, UC Berkeley, Stanford & many other of the World's finest University's.
Language: English
Professors: Michael Williams
Units: 42
Lesson content
- Mod-01 Lec-01 Introduction & Development of Jet Aircraft Propulsion
- Mod-01 Lec-02 How the Aircraft Jet Engines make Thrust
- Mod-01 Lec-03 Jet Engine Basic Performance Parameters
- Mod-01 Lec-04 Turbojet, Reheat Turbojet and Multi-spool Engines
- Mod-01 Lec-05 Turbofan, Turbo-prop and Turboshaft engines
- Mod-01 Lec-06 Ideal and Real Brayton cycles
- Mod-01 Lec-07 Jet Engine Cycles for Aircraft propulsion
- Mod-01 Lec-08 Cycle components and component performances
- Mod-01 Lec-09 Tute-1
- Mod-01 Lec-10 Analysis of engine real cycles
- Mod-01 Lec-11 Tute-2
- Mod-01 Lec-12 Thermodynamics of Compressors
- Mod-01 Lec-13 Thermodynamics of Turbines
- Mod-01 Lec-14 Axial Compressors : two dimensional analytical model
- Mod-01 Lec-15 Cascade analysis; Loss and Blade performance estimation
- Mod-01 Lec-16 Free Vortex theory; Single-Multi-stage characteristics
- Mod-01 Lec-17 Tutes -- 3
- Mod-01 Lec-18 Elements of centrifugal compressor
- Mod-01 Lec-19 Centrifugal Compressor characteristics: Surging, Choking
- Mod-01 Lec-20 Axial flow turbines; Turbine Blade 2-D (cascade) analysis
- Mod-01 Lec-21 Multi-staging: Axial Turbine; Turbine Cooling Technology
- Mod-01 Lec-22 Radial Turbine Aerodynamics & Thermodynamics; Losses
- Mod-01 Lec-23 Tutes -- 4
- Mod-01 Lec-24 Types of combustion chambers: mechanism & parameters
- Mod-01 Lec-25 Pr. Loss, Combustion efficiency; Combustion intensity
- Mod-01 Lec-26 Practical combustion system ; Stability, Fuel injection
- Mod-01 Lec-27 Intakes for Powerplant: Transport / Military Aircraft
- Mod-01 Lec-28 Subsonic, Transonic, Supersonic Intake Designs
- Mod-01 Lec-29 Nozzle : fixed and variable geometry nozzles
- Mod-01 Lec-30 C-D nozzle and their uses
- Mod-01 Lec-31 Tute-5
- Mod-01 Lec-32 Engine Off Design Operations
- Mod-01 Lec-33 Aircraft Engine component matching: Dimensional analysis
- Mod-01 Lec-34 Engine component matching and Sizing
- Mod-01 Lec-35 Installed Performance of Engine
- Mod-01 Lec-36 Tute-6
- Mod-01 Lec-37 Use of Ramjets and Pulsejets in Aircraft propulsion
- Mod-01 Lec-38 Thermodynamic Cycle & Performance Parameters
- Mod-01 Lec-39 Flow in Diffusers, Combustors and Nozzles
- Mod-01 Lec-40 Performanace and Design of Ramjet & Scramjet Engines
- Mod-01 Lec-41 Tute -- 7
- Mod-01 Lec-42 Future of Aircraft Propulsion
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