EY7202 DESIGN AND ANALYSIS OF TURBOMACHINES Syllabus

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Anna University Syllabus - Anna University ME Syllabus

EY7202 DESIGN AND ANALYSIS OF TURBOMACHINES Syllabus | Anna University ME Energy Engineering Second Semester Syllabus Regulation 2013. Below is the Anna University 2013 Regulation Syllabus for 2nd Semester for ME Energy engineering, Textbooks, Reference books, Exam portions, Question Bank, Previous year question papers, Model question papers, Class notes, Important 2 marks, 8 marks, 16 marks topics. 

It is applicable for all students admitted in the Academic year 2013-2014 onwards for all its Affiliated institutions in Tamil Nadu.


Anna University Chennai Syllabus


EY7202 DESIGN AND ANALYSIS OF TURBOMACHINES L T P C
3 0 0 3
AIM:
To design and analyse the performance of Turbo machines for engineering applications.
OBJECTIVES:
 To understand the energy transfer process in Turbomachines and governing equations of various
forms.
 To understand the structural and functional aspects of major components of Turbomachines.
 To design various Turbomachines for power plant and aircraft applications
UNIT I INTRODUCTION 12
Basics of isentropic flow – static and stagnation properties – diffuser and nozzle configurations - area
ratio – mass flow rate – critical properties. Energy transfer between fluid and rotor velocity triangles for
a generalized turbomachines - velocity diagrams. Euler's equation for turbomachines and its different
forms. Degree of reaction in turbo-machines – various efficiencies – isentropic, mechanical, thermal,
overall and polytropic
UNIT II CENTRIFUGAL AND AXIAL FLOW COMPRESSORS 9
Centrifugal compressor - configuration and working – slip factor - work input factor – ideal and actual
work - pressure coefficient - pressure ratio. Axial flow compressor – geometry and working – velocity
diagrams – ideal and actual work – stage pressure ratio - free vortex theory – performance curves and
losses
UNIT III COMBUSTION CHAMBER 6
Basics of combustion. Structure and working of combustion chamber – combustion chamber
arrangements - flame stability – fuel injection nozzles. Flame stabilization - cooling of combustion
chamber
UNIT IV AXIAL AND RADIAL FLOW TURBINES 9
Elementary theory of axial flow turbines - stage parameters- multi-staging - stage loading and flow
coefficients. Degree of reaction - stage temperature and pressure ratios – single and twin spool
arrangements – performance. Matching of components. Blade Cooling. Radial flow turbines.
UNIT V GAS TURBINE AND JET ENGINE CYCLES 9
Gas turbine cycle analysis – simple and actual. Reheated, Regenerative and Intercooled cycles for
power plants. Working of Turbojet, Turbofan, Turboprop, Ramjet, Scarmjet and Pulsejet Engines and
cycle analysis – thrust, specific impulse, specific fuel consumption, thermal and propulsive
efficiencies.
TOTAL: 45 PERIODS
OUTCOME:
When a student completes this subject, he / she can
 Understand the design principles of the turbomachines
 Analyse the turbomachines to improve and optimize its performance
REFERENCES
1. Ganesan, V., Gas Turbines, Tata McGrawHill, 2011.
2. Khajuria P.R and Dubey S.P., Gas Turbines and Propulsive Systems, Dhanpat Rai
Publications, 2003
3. Cohen, H., Rogers, G F C and Saravanmotto, H I H, Gas Turbine Theory, John Wiely, 5th
Edition 2001.
4. Hill P G and Peterson C R, Mechanics and Thermodynamics of Propulsion, Addition-Wesley,
1970.

5. Mattingly J D, Elements of Gas turbine Propulsion, McGraw Hill, 1st Edition. 1997