AKTU Aircraft Propulsion-II (BAE061) Syllabus PDF – B.Tech 3rd Year
Aircraft Propulsion-II BAE061
All syllabus, notes, question bank & PYQ for this subject
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- Semester 6
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Syllabus — Aircraft Propulsion-II
Download PDFBAE061 · 3 credits · L-T-P 3-0-0
| The students will be able to | Blooms Taxonomy | |
| CO-1 | Understand the working of turbojet, turboprop, turbofan and turbo-shaft engines and advantages and disadvantages, its applications. | K2 |
| CO-2 | Understand the jet propulsion is and how thrust is produced the working of turbofan, turbojet, turboprop and turbo-shaft engines. | K2 |
| CO-3 | Apply the concept of the energy transfer in turbo-machines and application of Euler momentum equation of. | K3 |
| CO-4 | Understand the characteristics and applications of different types of compressor and Principle of operations, design of radial blades, Analysis of work done and efficiencies. | K2 |
| CO-5 | Understand the process of combustion, types of combustors and related terminologies. Fuel injection atomization in simplex and duplex burners. | K2 |
| CO-6 | Apply the concept of the working of nozzles and inlets and their application in aircrafts & rockets. | K3 |
UNIT-I (8 Hours)
Introduction to Jet Engines Development of Jet Aircraft Propulsion, Turbojet, Turbofan, Turbo-prop & Turbo shaft, various components & working of jet engines, Ramjet and Scramjet engine Cycle Analysis Brayton cycle, Ideal & real cycle analysis of turbojet & ramjet engine, Performance, Thrust equation.
UNIT-II (9 Hours)
Basics of Turbo machinery Euler equation for turbo machinery and its significance, velocity triangles for a generalized turbo-machine, degree of reaction in turbo machines, free vortex and forced vortex.
Centrifugal compressor Characteristics and applications, various parts and their working, Principle of operation, Analysis of work done and efficiencies, compressibility effects, Design of diffuser, Pressure losses, surging, chocking, and degree of reaction, Comparison between axial compressor & centrifugal compressor.
UNIT-III (8 Hours)
Axial Compressor Characteristics and applications, parts of axial compressor. Principle of operation, two dimensional flow analyses, ideal and real work and efficiency of axial compressor, Analysis of Cascade effect & Losses, Factor effecting stage pressure, Blade design, stage performance estimation & off-design performance, compressibility effects, Degree of reaction, stalling, chocking & surging.
UNIT-IV (8 Hours)
Axial Turbine Characteristics and applications, Blade (cascade) profile analysis. Analysis of multi-staging axial Turbine, estimation of stage performance, Work done, efficiency & degree of reaction, Turbine Cooling Radial Turbine Characteristics and applications, aerodynamics & thermodynamics, Principle of operations, design of radial blades, Analysis of work done and efficiencies, estimation of stage performance degree of reaction, Stalling& surging, Losses.
UNIT-V (9 Hours)
Combustion Chamber Types of combustion systems, requirements, combustion process, mechanism & parameters, Combustion efficiency and intensity, losses, design of combustion chamber, combustion chamber performance, and Fuel injection atomization in simplex and duplex burners.
Nozzle Nozzle configurations, under and over expanded nozzles, mass flow through a nozzle. Theory of isentropic C-D nozzles, Types of nozzles, their application in aircrafts & rockets.
Books and Reference -
- Mechanics and Thermodynamics of Propulsion by Hill and Peterson.
- V. Ganesan, Gas Turbines, McGraw Hill Education
- H. Cohen and G.F.C Rogers, Saravanamutto, Gas Turbine Theory
- J. Mattingly, Elements of Propulsion, Tata McGraw Hill
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