ME2351 GAS DYNAMICS AND JET PROPULSION SYLLABUS | ANNA UNIVERSITY BE MECHANICAL ENGINEERING 6TH SEM SYLLABUS REGULATION 2008 2011 2012-2013 BELOW IS THE ANNA UNIVERSITY SIXTH SEMESTER BE MECHANICAL ENGINEERING DEPARTMENT SYLLABUS, TEXTBOOKS, REFERENCE BOOKS,EXAM PORTIONS,QUESTION BANK,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), 2008 REGULATION OF ANNA UNIVERSITY CHENNAI AND STUDENTS ADMITTED IN ANNA UNIVERSITY CHENNAI DURING 2009
ME2351 GAS DYNAMICS AND JET PROPULSION L T P C
3 1 0 4
AIM:
To impart knowledge to the students on compressible flow through ducts, jet propulsion
and space propulsion.
OBJECTIVE:
To understand the basic difference between incompressible and compressible flow.
To understand the phenomenon of shock waves and its effect on flow. To gain some
basic knowledge about jet propulsion and Rocket Propulsion.
UNIT I BASIC CONCEPTS AND ISENTROPIC FLOWS 6
Energy and momentum equations of compressible fluid flows – Stagnation states, Mach
waves and Mach cone – Effect of Mach number on compressibility – Isentropic flow
through variable ducts – Nozzle and Diffusers – Use of Gas tables.
UNIT II FLOW THROUGH DUCTS 9
Flows through constant area ducts with heat transfer (Rayleigh flow) and Friction (Fanno
flow) – variation of flow properties – Use of tables and charts – Generalised gas
dynamics.
55
UNIT III NORMAL AND OBLIQUE SHOCKS 10
Governing equations – Variation of flow parameters across the normal and oblique
shocks – Prandtl – Meyer relations – Use of table and charts – Applications.
UNIT IV JET PROPULSION 10
Theory of jet propulsion – Thrust equation – Thrust power and propulsive efficiency –
Operation principle, cycle analysis and use of stagnation state performance of ram jet,
turbojet, turbofan and turbo prop engines.
UNIT V SPACE PROPULSION 10
Types of rocket engines – Propellants-feeding systems – Ignition and combustion –
Theory of rocket propulsion – Performance study – Staging – Terminal and characteristic
velocity – Applications – space flights.
TUTORIALS: 15, TOTAL: 60 PERIODS
TEXT BOOKS:
1. Anderson, J.D., Modern Compressible flow, McGraw Hill, 3rd Edition, 2003.
2. H. Cohen, G.E.C. Rogers and Saravanamutto, Gas Turbine Theory, Longman Group
Ltd., 1980.
3. S.M. Yahya, fundamentals of Compressible Flow, New Age International (P) Limited,
New Delhi, 1996.
REFERENCES:
1. P. Hill and C. Peterson, Mechanics and Thermodynamics of Propulsion, Addison –
Wesley Publishing company, 1992.
2. N.J. Zucrow, Aircraft and Missile Propulsion, vol.1 & II, John Wiley, 1975.
3. N.J. Zucrow, Principles of Jet Propulsion and Gas Turbines, John Wiley, New York,
1970.
4. G.P. Sutton, Rocket Propulsion Elements, John wiley, 1986, New York.
5. A.H. Shapiro, Dynamics and Thermodynamics of Compressible fluid Flow, , John
wiley, 1953, New York.
6. V. Ganesan, Gas Turbines, Tata McGraw Hill Publishing Co., New Delhi, 1999.
7. PR.S.L. Somasundaram, Gas Dynamics and Jet Propulsions, New Age International
Publishers, 1996.
8. V. Babu, Fundamentals of Gas Dynamics, ANE Books India, 2008.
ME2351 GAS DYNAMICS AND JET PROPULSION L T P C
3 1 0 4
AIM:
To impart knowledge to the students on compressible flow through ducts, jet propulsion
and space propulsion.
OBJECTIVE:
To understand the basic difference between incompressible and compressible flow.
To understand the phenomenon of shock waves and its effect on flow. To gain some
basic knowledge about jet propulsion and Rocket Propulsion.
UNIT I BASIC CONCEPTS AND ISENTROPIC FLOWS 6
Energy and momentum equations of compressible fluid flows – Stagnation states, Mach
waves and Mach cone – Effect of Mach number on compressibility – Isentropic flow
through variable ducts – Nozzle and Diffusers – Use of Gas tables.
UNIT II FLOW THROUGH DUCTS 9
Flows through constant area ducts with heat transfer (Rayleigh flow) and Friction (Fanno
flow) – variation of flow properties – Use of tables and charts – Generalised gas
dynamics.
55
UNIT III NORMAL AND OBLIQUE SHOCKS 10
Governing equations – Variation of flow parameters across the normal and oblique
shocks – Prandtl – Meyer relations – Use of table and charts – Applications.
UNIT IV JET PROPULSION 10
Theory of jet propulsion – Thrust equation – Thrust power and propulsive efficiency –
Operation principle, cycle analysis and use of stagnation state performance of ram jet,
turbojet, turbofan and turbo prop engines.
UNIT V SPACE PROPULSION 10
Types of rocket engines – Propellants-feeding systems – Ignition and combustion –
Theory of rocket propulsion – Performance study – Staging – Terminal and characteristic
velocity – Applications – space flights.
TUTORIALS: 15, TOTAL: 60 PERIODS
TEXT BOOKS:
1. Anderson, J.D., Modern Compressible flow, McGraw Hill, 3rd Edition, 2003.
2. H. Cohen, G.E.C. Rogers and Saravanamutto, Gas Turbine Theory, Longman Group
Ltd., 1980.
3. S.M. Yahya, fundamentals of Compressible Flow, New Age International (P) Limited,
New Delhi, 1996.
REFERENCES:
1. P. Hill and C. Peterson, Mechanics and Thermodynamics of Propulsion, Addison –
Wesley Publishing company, 1992.
2. N.J. Zucrow, Aircraft and Missile Propulsion, vol.1 & II, John Wiley, 1975.
3. N.J. Zucrow, Principles of Jet Propulsion and Gas Turbines, John Wiley, New York,
1970.
4. G.P. Sutton, Rocket Propulsion Elements, John wiley, 1986, New York.
5. A.H. Shapiro, Dynamics and Thermodynamics of Compressible fluid Flow, , John
wiley, 1953, New York.
6. V. Ganesan, Gas Turbines, Tata McGraw Hill Publishing Co., New Delhi, 1999.
7. PR.S.L. Somasundaram, Gas Dynamics and Jet Propulsions, New Age International
Publishers, 1996.
8. V. Babu, Fundamentals of Gas Dynamics, ANE Books India, 2008.
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