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Course Detail

Course Name Turbomachinery
Course Code 25DT647
Program M.Tech. in Defence Technology
Semester 2
Credits 3
Campus Coimbatore

Syllabus

Syllabus

Course Content:

Unit

Contents

Contact Hrs.

1.

Introduction reviews about turbo machinery sub-system Velocity triangles. Efficiencies in Compressor and Turbine stages. Degree of reaction.

7

2.

Dimensionless parameters for Turbomachines. Concept of specific speed, shape number, axial, radial, and mixed flow machines, and similarity laws.

7

3.

Axial flow compressors: Introduction; Aero-Thermodynamics of flow through an Axial flow Compressor stage; Losses in axial flow compressor stage; Losses and Blade performance estimation; Secondary flows (3-D); Tip leakage flow and scrubbing; Simple three-dimensional flow analysis; rotating stall and surging.

6

4.

Centrifugal Compressors: Introduction; Elements of centrifugal compressor/ fan; Inlet Duct Impeller; Slip factor; Concept of Rothalpy; Modified work done; Incidence and lag angles; Diffuser ; Centrifugal Compressor Characteristics; Surging; Chocking; Rotating stall; Design

8

5.

Axial flow turbines – Introduction; Turbine stage; Turbine Blade 2-D (cascade) analysis Work Done; Degree of Reaction; Losses and Efficiency; Flow Passage; Subsonic, transonic and supersonic turbines, Multi-staging of Turbine; Exit flow conditions

6

6.

Turbine Cooling; Turbine Blade design – Turbine Profiles : Airfoil Data and Profile construction.

Radial flow turbines: Thermodynamics and Aerodynamics of radial turbines; Radial Turbine Characteristics; Losses and efficiency; Design of radial turbine.

6

7.

Aero-thermodynamics of Compressor-Turbine Systems; Aerodynamic and thermodynamic performance parameters; Optimization techniques for compressor-turbine matching.

5

Total

45

Objectives and Outcomes

Course Objectives:

The course is intended to enable the students to do design calculations for turbines and compressors as well as to carry out calculation of various performance parameters.

Course Outcomes:

At the end of the course the student should be able to:

  • Draw velocity triangles for turbomachines
  • Determine the key performance parameters for turbines and combustors
  • Analyze flow through axial and radial turbomachines
  • Carry out design calculations for turbines and compressors

Text Books / References

References / Suggested Books:

  • IGTI/ASME; The design of Gas Turbine Engines Thermodynamics and Aerodynamics (chapter 8 and 10), 2005.
  • Oates Gordon C; Aerothermodynamics of Aircraft Engine Components; AIAA series, 1985.
  • Dixon S. L. “Fluid Mechanics & Thermodynamics of Turbomachinery”, 6/e, Elsevier, 2012.
  • Principles of Turbo Machines/DG Shepherd / Macmillan, 1961.
  • Turbines, Pumps, Compressors/Yahya/ Mc Graw Hill, 4th Edition, 2011.
  • William W. Peng “Fundamentals of Turbomachinery” , John Wiley & Sons, 2007.

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