Aerospace - Jet Aircraft Propulsion

Total Lectures


Mod-01 Lec-01 Introduction & Development of Jet Aircraft Propulsion


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 Development of Jet propulsion for aircraft
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-02 Lec-22 Radial Turbine Aerodynamics & Thermodynamics; Losses
Mod-03 Lec-23 Tutes – 4
Mod-04 Lec-24 Types of combustion chambers: mechanism & parameters
Mod-05 Lec-25 Pr. Loss, Combustion efficiency; Combustion intensity
Mod-06 Lec-26 Practical combustion system ; Stability, Fuel injection
Mod-07 Lec-27 Intakes for Powerplant: Transport / Military Aircraft
Mod-08 Lec-28 Subsonic, Transonic, Supersonic Intake Designs
Mod-09 Lec-29 Nozzle : fixed and variable geometry nozzles
Mod-10 Lec-30 C-D nozzle and their uses
Mod-11 Lec-31 Tute-5
Mod-12 Lec-32 Engine Off Design Operations
Mod-13 Lec-33 Aircraft Engine component matching: Dimensional analysis
Mod-14 Lec-34 Engine component matching and Sizing
Mod-15 Lec-35 Installed Performance of Engine
Mod-16 Lec-36 Tute-6
Mod-17 Lec-37 Use of Ramjets and Pulsejets in Aircraft propulsion
Mod-18 Lec-38 Thermodynamic Cycle & Performance Parameters
Mod-19 Lec-39 Flow in Diffusers, Combustors and Nozzles
Mod-20 Lec-40 Performanace and Design of Ramjet & Scramjet Engines
Mod-21 Lec-41 Tute – 7
Mod-22 Lec-42 Future of Aircraft Propulsion
Mod-01 Lec-03 Jet Engine Basic Performance Parameters
OER.UoCh.Edu.Pk (University of Chitral Open Educational Resources).

In the wake of the global emergency on Novel Coronavirus (COVID-19), the universities of Pakistan are planning to go online under the aegis of the Higher Education Commission of Pakistan (HEC). The University of Chitral has launched a comprehensive open learning knowledge hub to assist the faculty and students both at home and abroad to learn through the web. This includes a wide range of learning resources including free audio-visual lectures from the top universities and institutes of the world.