Jet Aircraft Propulsion detail syllabus for Aeronautical Engineering (Aero), 2019-20 scheme is taken from AKTU official website and presented for AKTU students. The course code (RAE061), and for exam duration, Teaching Hr/Week, Practical Hr/Week, Total Marks, internal marks, theory marks, and credits do visit complete sem subjects post given below.
For all other aero 6th sem syllabus for b.tech 2019-20 scheme aktu you can visit Aero 6th Sem syllabus for B.Tech 2019-20 Scheme AKTU Subjects. For all other Departmental Elective-2 subjects do refer to Departmental Elective-2. The detail syllabus for jet aircraft propulsion is as follows.
Unit 1
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Unit 2
Euler turbine equation and its different forms,velocity triangles for a generalized turbo- machine degree of reaction in turbo machines, methods of representing velocity diagrams. velocity triangle for a stage radial equilibrium, free vortex, forced vortex and constant reaction designs; variation of blade height for the above types of blades, allowable temperature and pressure rise per stage; blade nomenclature, pressure loss coefficient , lift and drag, losses in blade passages, stall and surge, simple design examples.
Unit 3
Thermodynamics of Compressors and their characteristics and applications.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 and losses. Analysis of work done and efficiencies of compressors.
Unit 4
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Unit 5
Combustion Chamber-Types of combustion chambers: mechanism & parameters. Loss, Combustion efficiency; Combustion intensity.Practical combustion system; Stability.Intakes for Power plant: Transport/Military Aircraft. Requirement of a combustion chamber, Aerodynamic and chemical performance of combustion chambers. Balance energy equation. Effect of operating conditions of the performance of combustion chambers.Cooling of Flame tubes and
Fuel injection and control systems. Fuel injection atomization in simplex and duplex burners. All type of C-D Nozzles fixed and variable geometry, their operations characteristics at various altitudes and speeds their uses and Subsonic, Transonic, Supersonic Intake Designs.
Books and References:
- Mechanics and Thermodynamics of Propulsion by Hill and Peterson,
- Jet Propulsion for Aerospace Application by Hesse and Mumford,
- Aircraft and Missile Propulsion by M,J, Zucrow, Vols, I and it,
- The theory and Design of Gas Turbines and Jet Engines by E,T, Vincent,
- Gas Turbine Theory by H, Cohen and G,F,C, Rogers,
For detail syllabus of all other subjects of B.Tech Aero, 2019-20 regulation do visit Aero 6th Sem syllabus for 2019-20 Regulation.
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