Turbo Machinery detailed syllabus for Aeronautical Engineering (AERO), R18 regulation has been taken from the JNTUHs official website and presented for the students of B.Tech Aeronautical Engineering branch affiliated to JNTUH course structure. For Course Code, Course Titles, 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 the other AERO 4th Year 1st Sem Syllabus for B.Tech R18 Regulation JNTUH scheme, visit Aeronautical Engineering 4th Year 1st Sem R18 Scheme.
For all the (Professional Elective-4) subjects refer to Professional Elective-4 Scheme. The detail syllabus for turbo machinery is as follows.
Pre-requisites:
Thermal Engineering, Heat Transfer
Course Objective:
For the complete syllabus, results, class timetable, and many other features kindly download the iStudy App
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Course Outcome:
- Ability to design and calculate different parameters for turbo machines
- PRErequisite to CFD and Industrial fluid power courses
- Ability to formulate design criteria
- Ability to understand thermodynamics and kinematics behind turbo machines
Unit – I
Introduction to Turbomachinery: Classification of turbo-machines, second law of thermodynamics applied to turbine and compressors work, nozzle, diffuser work, fluid equation, continuity, Euler�s, Bernoulli�s, equation and its applications, expansion and compression process, reheat factor, preheat factor
Unit – II
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Unit – III
Gas Dynamics: Fundamental thermodynamic concepts, isentropic conditions, mach numbers, and area, Velocity relations, Dynamic Pressure, Normal shock relation for perfect gas. Supersonic flow, oblique shock waves. Normal shock recoveries, detached shocks, Aerofoil theory. Centrifugal compressor: Types, Velocity triangles and efficiencies, Blade passage design, Diffuser and pressure recovery. Slip factor, Stanitz and Stodolas formulas, Effect of inlet mach numbers, Pre whirl, Performance
Unit – IV
Axial Flow Compressors: Flow Analysis, Work, and velocity triangles, Efficiencies, Thermodynamic analysis. Stage pressure rise, Degree of reaction, Stage Loading, General design, Effect of velocity, Incidence, Performance Cascade Analysis: Geometrical and terminology. Blade force, Efficiencies, Losses, Free end force, Vortex Blades.
Unit – V
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Text Books:
- Principles of Turbo Machines/DG Shepherd / Macmillan
- Turbines, Pumps, Compressors/Yahya/ Mc Graw Hill
Reference Books:
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..
For detail syllabus of all other subjects of B.Tech Aeronautical Engineering 4th Year 1st Sem , visit AERO 4th Year 1st Sem syllabus subjects.
For B.Tech Aeronautical Engineering (AERO) 4th Year results, visit JNTUH B.Tech Aeronautical Engineering semester results direct link.