Aircraft Propulsion detailed Syllabus for Aeronautical Engineering (AERO), 2018 scheme has been taken from the VTUs official website and presented for the VTU students. For Course Code, Subject Names, Teaching Department, Paper Setting Board, Theory Lectures, Tutorial, Practical/Drawing, Duration in Hours, CIE Marks, Total Marks, Credits and other information do visit full semester subjects post given below. The Syllabus PDF files can also be downloaded from the official website of the university.
For all other VTU AERO 4th Sem Syllabus for BE 2018 Scheme, do visit VTU AERO 4th Sem Syllabus for BE 2018 Scheme Subjects. The detailed Syllabus for aircraft propulsion is as follows.
Course Objectives:
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Module 1
Introduction: Review of thermodynamic principles, Principles of aircraft propulsion, Types of power plants, Working principles of internal combustion engine, Two-stroke and four-stroke piston engines, Gas- turbine engines, Cycle analysis of reciprocating engines and jet engines , advantages and disadvantages.
Module 2
Propeller Theories & Jet propulsion Types of propeller, Propeller thrust: momentum theory, Blade element theories, propeller blade design, propeller selection. Jet Propulsion: Illustration of working of gas turbine engine-The thrust equation-Factors affecting thrust -Effect of pressure, velocity and temperature changes of air entering compressor-Methods of thrust augmentation-Characteristics of turboprop, turbofan and turbojet-Performance characteristics.
Module 3
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Module 4
Gas Turbine Engine Compressors Centrifugal compressors: Principle of operation of centrifugal compressors. Work done and pressure rise -Velocity diagrams, Diffuser vane design considerations. performance characteristics. Concept of Pre-whirl, Rotating stall. Axial flow compressors: Elementary theory of axial flow compressor, Velocity triangles, Degree of reaction, three-dimensional flow. Air angle distribution for free vortex and constant reaction designs, Compressor blade design. Axial compressor performance characteristics.
Module 5
Combustion chambers and Turbines Classification of combustion chambers, important factors affecting combustion chamber design, Combustion process, Combustion chamber performance Effect of operating variables on performance-Flame tube cooling-Flame stabilization-Use of flame holders Axial Flow Turbines: Introduction, Turbine stage, Multi-staging of turbine, Exit flow conditions, Turbine cooling, Heat transfer in turbine cooling. Radial turbine: Introduction, Thermodynamics of radial turbines, Losses and efficiency.
Course Outcomes:
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Question paper pattern:
- The question paper will have ten full questions carrying equal marks. Each full question consisting of 20 marks.
- There will be two full questions (with a maximum of four sub questions) from each module.
- Each full question will have sub question covering all the topics under a module.
- The students will have to answer five full questions, selecting one full question from each module.
Text Books:
- Aircraft propulsion Bhaskar Roy Elsevier 2011
- Gas Turbines V. Ganesan Tata McGraw-Hill 2010
Reference Books:
For the complete Syllabus, results, class timetable, and many other features kindly download the iStudy App
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For detail Syllabus of all other subjects of BE 4th Sem Aeronautical Engineering, visit (AERO) 4th Sem Syllabus Subjects.
For all (CBSE & Non-CBSC) BE results, visit VTU BE all semester results direct links.