Aircraft Propulsion detailed Syllabus for Aeronautical Engineering (AERO), R18 regulation has been taken from the JNTUH official website and presented for the students affiliated to JNTUH course structure. For Course Code, Subject Names, Theory Lectures, Tutorial, Practical/Drawing, Credits, and other information do visit full semester subjects post given below. The Syllabus PDF files can also be downloaded from the universities official website.
For all other AERO 3rd Year 1st Sem Syllabus for B.Tech R18 Regulation JNTUH, do visit AERO 3rd Year 1st Sem Syllabus for B.Tech R18 Regulation JNTUH Subjects. The detailed Syllabus for aircraft propulsion is as follows.
Pre-requisite:
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Course Objectives:
- Analyse parametric cyclic analysis, performance parameters, efficiency, specific impulse of all air breathing engines.
- Know the design and performance of subsonic and supersonic inlets, types of combustion chambers and factors affecting the combustors.
- Discuss the types of nozzles, flow conditions in nozzles, interaction of nozzle flow with adjacent surfaces and thrust reversal
- Explain different types of compressors and turbines, work done, velocity diagrams and stage efficiency calculations.
Course Outcomes:
- Review the basic thermodynamic principles and fundamentals of gas turbine engines
- Outline the concepts of subsonic and supersonic inlets for jet engines
- Evaluate the operating characteristics of compressors and turbines in terms of blade shapes, angles, and direction of rotation
- Describe the fundamentals of combustion chamber, nozzle, ramjet and rocket propulsion
Unit I
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Unit II
Inlets And Combustion Chambers: Internal flow and stall in subsonic inlets, relation between minimum area ratio and eternal deceleration ratio, diffuser performance, supersonic inlets, starting problem on supersonic inlets, shock swallowing by area variation; Classification of combustion chambers, combustion chamber performance, effect of operating variables on performance, flame stabilization.
Unit III
Nozzles: Theory of flow in isentropic nozzles, nozzles and choking, nozzle throat conditions, nozzle efficiency, losses in nozzles. Over expanded and under expanded nozzles, ejector and variable area nozzles, interaction of nozzle flow with adjacent surfaces, thrust reversal.
Unit IV
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Unit V
Turbines: Principle of operation of axial flow turbines, limitations of radial flow turbines, work done and pressure rise, velocity triangles, degree of reaction, free vortex and constant angle designs, performance characteristics, sample ramjet design calculations, flame stability problems in ramjet combustors, integral ram rockets.
Text Books:
- Hill, P.G. and Peterson, C.R. Mechanics and Thermodynamics of Propulsion! Addison Wesley Longman INC, 1999.
- Mattingly J.D., Elements of Propulsion: Gas Turbines and Rocketll, AIAA, 1991.
Reference Book:
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 B.Tech 3rd Year Aeronautical Engineering, visit AERO 3rd Year Syllabus Subjects.
For all B.Tech results, visit JNTUH B.Tech all years, and semester results from direct links.