AE2304 PROPULSION – II SYLLABUS | ANNA UNIVERSITY BE AERONAUTICAL ENGINEERING 5TH SEMESTER SYLLABUS REGULATION 2008 2011 2012-2013 BELOW IS THE ANNA UNIVERSITY FIFTH SEMESTER BE AERONAUTICAL ENGINEERING DEPARTMENT SYLLABUS IT IS APPLICABLE FOR ALL STUDENTS ADMITTED IN THE YEAR 2011 2012-2013 (ANNA UNIVERSITY CHENNAI,TRICHY,MADURAI,TIRUNELVELI,COIMBATORE), 2008 REGULATION OF ANNA UNIVERSITY CHENNAI AND STUDENTS ADMITTED IN ANNA UNIVERSITY CHENNAI DURING 2009
AE2304 PROPULSION – II L T P C
3 0 0 3
OBJECTIVE
To study in detail about gas turbines, ramjet, fundamentals of rocket propulsion and
chemical rockets
UNIT I AIRCRAFT GAS TURBINES 12
Impulse and reaction blading of gas turbines – Velocity triangles and power output –
Elementary theory – Vortex theory – Choice of blade profile, pitch and chord – Estimation
of stage performance – Limiting factors in gas turbine design- Overall turbine performance
– Methods of blade cooling – Matching of turbine and compressor.
45
UNIT II RAMJET PROPULSION: 8
Operating principle – Sub critical, critical and supercritical operation – Combustion in
ramjet engine – Ramjet performance – Simple ramjet design calculations – Introduction to
scramjet.
UNIT III FUNDAMENTALS OF ROCKET PROPULSION 8
Operating principle – Specific impulse of a rocket – internal ballistics- Rocket nozzle
classification – Rocket performance considerations.
UNIT IV CHEMICAL ROCKETS 12
Solid propellant rockets – Selection criteria of solid propellants – Important hardware
components of solid rockets – Propellant grain design considerations – Liquid propellant
rockets – Selection of liquid propellants. Cooling in liquid rockets – Hybrid rockets.
UNIT V ADVANCED PROPULSION TECHNIQUES 5
Electric rocket propulsion – Ion propulsion techniques – Nuclear rocket – Types – Solar
sail- Preliminary Concepts in nozzleless propulsion.
TOTAL: 45 PERIODS
TEXT BOOKS
1. Sutton, G.P., “Rocket Propulsion Elements”, John Wiley & Sons Inc., New York, 5th
Edn., 1993.
2. Hill, P.G. & Peterson, C.R. “Mechanics & Thermodynamics of Propulsion” Addison –
Wesley Longman INC, 1999.
REFERENCES
1. Cohen, H., Rogers, G.F.C. and Saravanamuttoo, H.I.H., “Gas Turbine Theory”,
Longman Co., ELBS Ed., 1989.
2. Gorden, C.V., “Aero thermodynamics of Gas Turbine and Rocket Propulsion”, AIAA
Education Series, New York, 1989.
3. Mathur, M., and Sharma, R.P., “Gas Turbines and Jet and Rocket Propulsion”,
Standard Publishers, New Delhi, 1988.
AE2304 PROPULSION – II L T P C
3 0 0 3
OBJECTIVE
To study in detail about gas turbines, ramjet, fundamentals of rocket propulsion and
chemical rockets
UNIT I AIRCRAFT GAS TURBINES 12
Impulse and reaction blading of gas turbines – Velocity triangles and power output –
Elementary theory – Vortex theory – Choice of blade profile, pitch and chord – Estimation
of stage performance – Limiting factors in gas turbine design- Overall turbine performance
– Methods of blade cooling – Matching of turbine and compressor.
45
UNIT II RAMJET PROPULSION: 8
Operating principle – Sub critical, critical and supercritical operation – Combustion in
ramjet engine – Ramjet performance – Simple ramjet design calculations – Introduction to
scramjet.
UNIT III FUNDAMENTALS OF ROCKET PROPULSION 8
Operating principle – Specific impulse of a rocket – internal ballistics- Rocket nozzle
classification – Rocket performance considerations.
UNIT IV CHEMICAL ROCKETS 12
Solid propellant rockets – Selection criteria of solid propellants – Important hardware
components of solid rockets – Propellant grain design considerations – Liquid propellant
rockets – Selection of liquid propellants. Cooling in liquid rockets – Hybrid rockets.
UNIT V ADVANCED PROPULSION TECHNIQUES 5
Electric rocket propulsion – Ion propulsion techniques – Nuclear rocket – Types – Solar
sail- Preliminary Concepts in nozzleless propulsion.
TOTAL: 45 PERIODS
TEXT BOOKS
1. Sutton, G.P., “Rocket Propulsion Elements”, John Wiley & Sons Inc., New York, 5th
Edn., 1993.
2. Hill, P.G. & Peterson, C.R. “Mechanics & Thermodynamics of Propulsion” Addison –
Wesley Longman INC, 1999.
REFERENCES
1. Cohen, H., Rogers, G.F.C. and Saravanamuttoo, H.I.H., “Gas Turbine Theory”,
Longman Co., ELBS Ed., 1989.
2. Gorden, C.V., “Aero thermodynamics of Gas Turbine and Rocket Propulsion”, AIAA
Education Series, New York, 1989.
3. Mathur, M., and Sharma, R.P., “Gas Turbines and Jet and Rocket Propulsion”,
Standard Publishers, New Delhi, 1988.
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