CY9008 GAS TURBINES AND JET PROPULSION SYLLABUS | ANNA UNIVERSITY ME CRYOGENIC ENGINEERING ELECTIVES SYLLABUS REGULATION 2009 2011 2012-2013 BELOW IS THE ANNA UNIVERSITY M.E CRYOGENIC ENGINEERING DEPARTMENT ELECTIVES SYLLABUS, 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 YEAR 2011 2012-2013 (ANNA UNIVERSITY CHENNAI,TRICHY,MADURAI,TIRUNELVELI,COIMBATORE), 2009 REGULATION OF ANNA UNIVERSITY CHENNAI AND STUDENTS ADMITTED IN ANNA UNIVERSITY CHENNAI DURING 2010
CY9008 GAS TURBINES AND JET PROPULSION L T P C
3 0 0 3
UNIT I GAS TURBINE CYCLES 10
Gas turbine cycles – Air Standard Analysis, Different configurations – Re-heater,
Intercooler, Heat Exchanger; Component behaviour.
UNIT II AXIAL FLOW COMPRESSORS 9
Momentum and energy transfer in rotors - Velocity triangles - Stage performance -
Degree of reaction - Three-dimensional analysis - Cascade testing - Compressor
characteristic curves – Howell’s Correlation - Surging and stalling.
Stage velocity triangles - impulse and reaction turbines, losses and co-efficient - blade design
principles - three-dimensional analysis - testing and performance characteristics
– Compounding methods - blade cooling.
UNIT III CENTRIFUGAL COMPRESSORS AND RADIAL TURBINES 10
Construction and wo r k in g principle - velocity triangles - backward, forward and radially
swept blades - losses and coefficients- performance characteristics. Types of inward flow
radial (IFR) turbine – velocity triangles – thermodynamics of the 900 IFR turbine –
optimum design solution of 900 IFR turbines – stage losses –performance
characteristics.
UNIT IV THERMODYNAMICS OF AIRCRAFT ENGINES 9
Theory of Aircraft propulsion – Thrust – Various efficiencies – Different propulsion
systems – Turboprop – Ram Jet – Turbojet, Turbojet with after burner, Turbo fan and Turbo
shaft. Engine – Aircraft matching – Design of inlets and nozzles – Performance characteristics
of Ramjet, Turbojet, Scramjet and Turbofan engines.
UNIT V ROCKET PROPULSION 9
Theory of rocket propulsion – Rocket equations – Escape and Orbital velocity – Multistaging
of Rockets – Space missions – Performance characteristics – Losses and
efficiencies.
Combustion in solid and liquid propellant rockets – Classification of propellants and
Propellant Injection systems – Non-equilibrium expansion and supersonic combustion –
Propellant feed systems – Reaction Control Systems – Rocket heat transfer.
TOTAL : 45 PERIODS
TEXT BOOKS:
1. Cohen, H., Rogers, G.E.C., and Saravanamuttoo, H.I.H., Gas Turbine Theory, Longman
Group Ltd, 1989.
2. Philip G . Hill a n d Carl R . P e t e r s o n , Mechanics and Thermodynamics o f
Propulsion, Second Edition, Addition – Wesley Publishing Company, New York, 1992.
3. Zucrow N.J. Principles of Jet Propulsion and Gas Turbines, John Wiley and Sons Inc, New
York, 1970.
4. Zucrow N.J. Aircraft and Missile Propulsion, Vol. I and Vol. II, John Wiley and Sons Inc,
New York, 1975.
CY9008 GAS TURBINES AND JET PROPULSION L T P C
3 0 0 3
UNIT I GAS TURBINE CYCLES 10
Gas turbine cycles – Air Standard Analysis, Different configurations – Re-heater,
Intercooler, Heat Exchanger; Component behaviour.
UNIT II AXIAL FLOW COMPRESSORS 9
Momentum and energy transfer in rotors - Velocity triangles - Stage performance -
Degree of reaction - Three-dimensional analysis - Cascade testing - Compressor
characteristic curves – Howell’s Correlation - Surging and stalling.
Stage velocity triangles - impulse and reaction turbines, losses and co-efficient - blade design
principles - three-dimensional analysis - testing and performance characteristics
– Compounding methods - blade cooling.
UNIT III CENTRIFUGAL COMPRESSORS AND RADIAL TURBINES 10
Construction and wo r k in g principle - velocity triangles - backward, forward and radially
swept blades - losses and coefficients- performance characteristics. Types of inward flow
radial (IFR) turbine – velocity triangles – thermodynamics of the 900 IFR turbine –
optimum design solution of 900 IFR turbines – stage losses –performance
characteristics.
UNIT IV THERMODYNAMICS OF AIRCRAFT ENGINES 9
Theory of Aircraft propulsion – Thrust – Various efficiencies – Different propulsion
systems – Turboprop – Ram Jet – Turbojet, Turbojet with after burner, Turbo fan and Turbo
shaft. Engine – Aircraft matching – Design of inlets and nozzles – Performance characteristics
of Ramjet, Turbojet, Scramjet and Turbofan engines.
UNIT V ROCKET PROPULSION 9
Theory of rocket propulsion – Rocket equations – Escape and Orbital velocity – Multistaging
of Rockets – Space missions – Performance characteristics – Losses and
efficiencies.
Combustion in solid and liquid propellant rockets – Classification of propellants and
Propellant Injection systems – Non-equilibrium expansion and supersonic combustion –
Propellant feed systems – Reaction Control Systems – Rocket heat transfer.
TOTAL : 45 PERIODS
TEXT BOOKS:
1. Cohen, H., Rogers, G.E.C., and Saravanamuttoo, H.I.H., Gas Turbine Theory, Longman
Group Ltd, 1989.
2. Philip G . Hill a n d Carl R . P e t e r s o n , Mechanics and Thermodynamics o f
Propulsion, Second Edition, Addition – Wesley Publishing Company, New York, 1992.
3. Zucrow N.J. Principles of Jet Propulsion and Gas Turbines, John Wiley and Sons Inc, New
York, 1970.
4. Zucrow N.J. Aircraft and Missile Propulsion, Vol. I and Vol. II, John Wiley and Sons Inc,
New York, 1975.
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