Module Name | Download | Description | Download Size |
---|---|---|---|
Jet Aircraft Propulsion | Lect-01 | Introduction of course | 1217 |
Jet Aircraft Propulsion | Lect-02 | How the thrust is created for flying | 1694 |
Jet Aircraft Propulsion | Lect-03 | Jet Engine Thrust and Other Performance Parameters | 1031 |
Jet Aircraft Propulsion | Lect-04 | Performance of a basic Jet engine | 894 |
Jet Aircraft Propulsion | Lect-05 | Variants of Aircraft Jet Engines | 2131 |
Jet Aircraft Propulsion | Lect-06 | Brayton cycles | 196 |
Jet Aircraft Propulsion | Lect-07 | Jet engine cycles for aircraft propulsion | 208 |
Jet Aircraft Propulsion | Lect-08 | Cycle components and component performance | 257 |
Jet Aircraft Propulsion | Lect-10 | Real cycle analysis | 234 |
Jet Aircraft Propulsion | Lect-12 | Thermodynamics of Compressors | 1294 |
Jet Aircraft Propulsion | Lect-13 | Thermodynamics of Turbines | 512 |
Jet Aircraft Propulsion | Lect-14 | Axial flow compressors | 258 |
Jet Aircraft Propulsion | Lect-15 | Cascade analysis | 495 |
Jet Aircraft Propulsion | Lect-16 | Free vortex theory Single and multi-stage axial compressor characteristics | 496 |
Jet Aircraft Propulsion | Lect-18 | Elements of centrifugal compressors | 529 |
Jet Aircraft Propulsion | Lect-19 | Performance characteristics of centrifugal compressors Surging and choking | 290 |
Jet Aircraft Propulsion | Lect-20 | Axial Flow Turbine Aerothermodynamic Fundamentals | 369 |
Jet Aircraft Propulsion | Lect-21 | Axial Turbine | 1258 |
Jet Aircraft Propulsion | Lect-22 | Radial Flow Turbines | 1672 |
Jet Aircraft Propulsion | Lect-24 | Combustion Chambers, Combustion Mechanism | 784 |
Jet Aircraft Propulsion | Lect-25 | Combustion Parameters | 257 |
Jet Aircraft Propulsion | Lect-26 | Combustion | 409 |
Jet Aircraft Propulsion | Lect-27 | Intakes for Transport aircraft,Military aircraft | 505 |
Jet Aircraft Propulsion | Lect-28 | Performance of intakes | 616 |
Jet Aircraft Propulsion | Lect-29 | Nozzle | 676 |
Jet Aircraft Propulsion | Lect-30 | Subsonic and supersonic nozzles, Working of these nozzles, Performance parameters for nozzles | 239 |
Jet Aircraft Propulsion | Lect-32 | Off-Design Operation Of Aircraft Jet Engines | 1230 |
Jet Aircraft Propulsion | Lect-33 | Matching of Engine Components | 731 |
Jet Aircraft Propulsion | Lect-34 | Engine Component Matching and Sizing | 722 |
Jet Aircraft Propulsion | Lect-35 | Installed performance of Engines | 395 |
Jet Aircraft Propulsion | Lect-37 | Ramjets and Pulsejets in Aircraft Propulsion | 469 |
Jet Aircraft Propulsion | Lect-38 | Thermodynamic cycle and performance parameters of ramjets and pulsejets | 188 |
Jet Aircraft Propulsion | Lect-39 | Components of ramjets and pulsejets | 244 |
Jet Aircraft Propulsion | Lect-40 | Performance of Ramjet Engines | 1211 |
Sl.No | Chapter Name | English |
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1 | L1-Introduction & Development of Jet Aircraft Propulsion | PDF unavailable |
2 | L2-How the Aircraft Jet Engines make Thrust | PDF unavailable |
3 | L3-Jet Engine Basic Performance Parameters | PDF unavailable |
4 | L4-Turbojet, Reheat Turbojet and Multi-spool Engines | PDF unavailable |
5 | L5-Turbofan, Turbo-prop and Turboshaft engines | PDF unavailable |
6 | L6-Ideal and Real Brayton cycles | PDF unavailable |
7 | L7-Jet Engine Cycles for Aircraft propulsion | PDF unavailable |
8 | L8-Cycle components and component performances | PDF unavailable |
9 | L9-Tute-1 | PDF unavailable |
10 | L10-Analysis of engine real cycles | PDF unavailable |
11 | L11-Tute-2 | PDF unavailable |
12 | L12-Thermodynamics of Compressors | PDF unavailable |
13 | L13-Thermodynamics of Turbines | PDF unavailable |
14 | L14-Axial Compressors : two dimensional analytical model | PDF unavailable |
15 | L15-Cascade analysis; Loss and Blade performance estimation | PDF unavailable |
16 | L16-Free Vortex theory; Single-Multi-stage characteristics | PDF unavailable |
17 | L17-Tutes – 3 | PDF unavailable |
18 | L18-Elements of centrifugal compressor | PDF unavailable |
19 | L19-Centrifugal Compressor characteristics: Surging, Choking | PDF unavailable |
20 | L20-Axial flow turbines; Turbine Blade 2-D (cascade) analysis | PDF unavailable |
21 | L21-Multi-staging: Axial Turbine; Turbine Cooling Technology | PDF unavailable |
22 | L22-Radial Turbine Aerodynamics & Thermodynamics; Losses | PDF unavailable |
23 | L23-Tutes – 4 | PDF unavailable |
24 | L24-Types of combustion chambers: mechanism & parameters | PDF unavailable |
25 | L25-Pr. Loss, Combustion efficiency; Combustion intensity | PDF unavailable |
26 | L26-Practical combustion system ; Stability, Fuel injection | PDF unavailable |
27 | L27-Intakes for Powerplant: Transport / Military Aircraft | PDF unavailable |
28 | L28-Subsonic, Transonic, Supersonic Intake Designs | PDF unavailable |
29 | L29-Nozzle : fixed and variable geometry nozzles | PDF unavailable |
30 | L30-C-D nozzle and their uses | PDF unavailable |
31 | L31-Tute-5 | PDF unavailable |
32 | L32-Engine Off Design Operations | PDF unavailable |
33 | L33-Aircraft Engine component matching: Dimensional analysis | PDF unavailable |
34 | L34-Engine component matching and Sizing | PDF unavailable |
35 | L35-Installed Performance of Engine | PDF unavailable |
36 | L36-Tute-6 | PDF unavailable |
37 | L37-Use of Ramjets and Pulsejets in Aircraft propulsion | PDF unavailable |
38 | L38-Thermodynamic Cycle & Performance Parameters | PDF unavailable |
39 | L39-Flow in Diffusers, Combustors and Nozzles | PDF unavailable |
40 | L40-Performanace and Design of Ramjet & Scramjet Engines | PDF unavailable |
41 | L41-Tute – 7 | PDF unavailable |
42 | L42-Future of Aircraft Propulsion | PDF unavailable |
Sl.No | Language | Book link |
---|---|---|
1 | English | Not Available |
2 | Bengali | Not Available |
3 | Gujarati | Not Available |
4 | Hindi | Not Available |
5 | Kannada | Not Available |
6 | Malayalam | Not Available |
7 | Marathi | Not Available |
8 | Tamil | Not Available |
9 | Telugu | Not Available |