Design of Gas Turbine Engine Components detailed syllabus for Aeronautical Engineering (Aero) for 2019 regulation curriculum has been taken from the Anna Universities official website and presented for the Aero students. For course code, course name, number of credits for a course and other scheme related information, do visit full semester subjects post given below.
For Aeronautical Engineering 6th Sem scheme and its subjects, do visit Aero 6th Sem 2019 regulation scheme. For Professional Elective-II scheme and its subjects refer to Aero Professional Elective-II syllabus scheme. The detailed syllabus of design of gas turbine engine components is as follows.
Course Objective:
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Unit I
Gas Turbine Engine Design Fundamentals
Design Process- compressible flow relationship; Constraint Analysis – Concept-Design tools-preliminary estimates; Mission analysis – Aircraft weight and fuel consumption data-Example problems on Constrain analysis, Mission analysis.
Unit II
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Unit III
Design of Rotating Components
Fan and Compressor Aerodynamics-Diffusion factor-Aerofoil geometry-Flow path dimensionRadial variation-Turbine Aerodynamics- Constant axial velocity-adiabatic-selected Mach number-Mean line stage Design-stage pressure ratio-Airfoil geometry-radial variation-turbine cooling-range of turbine parameters-Engine life-Design Example -for fan-compressor-turbine.
Unit IV
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Unit V
Inlet and Nozzle Design
Inlets and Exhaust Nozzles Design: Elements of a Successful Inlet-Engine Integration Program-Definition of Subsonic Inlet-Engine Operational Requirements- Definition of Supersonic Inlet-Engine Operational Requirements- Engine Impact on Inlet Design- Inlet Impact on Engine Design-Validation of Inlet-Engine System-Exhaust nozzle design-Nozzle types and their design -Jet control methods for reduction of infrared signature.
Course Outcome:
For the complete syllabus, results, class timetable, and many other features kindly download the iStudy App
It is a lightweight, easy to use, no images, and no pdfs platform to make students’s lives easier..
Text Books:
- Mattingly J.D., Heiser, W.H. and Pratt D.T, Aircraft Engine Design, 2nd Edition, AIAA Education Series, AIAA, 2002.
- Oates G.C., Aircraft Propulsion Systems Technology and Design,1989, AIAA Education Series.
- Saravanamuttoo H.I.H and Rogers, G.F.C. “Gas Turbine Technology”, Pearson Education Canada; 6th edition, 2008.
References:
- Cumpsty N., “Jet Propulsion: A Simple Guide to the Aerodynamics and Thermodynamics Design and Performance of Jet Engines” , Cambridge University Press; 2nd edition, 2003
- Murthy S.N. and Curran E.T., High-Speed Flight Propulsion Systems, Volume 137, Progress in Astronautics and Aeronautics, AIAA,1991.
- Rathakrishnan E, Applied Gas Dynamics, John Wiley and Sons (Asia) Pvt Ltd, 2010.
- Treage I.E, Aircraft Gas Turbine Engine Technology, 3rd edition, Glencoe McGraw-Hill, Inc. 1995
For detailed syllabus of all the other subjects of Aeronautical Engineering 6th Sem, visit Aero 6th Sem subject syllabuses for 2019 regulation.
For all Aeronautical Engineering results, visit Anna University Aero all semester results direct link.