## ME6604 GAS DYNAMICS AND JET PROPULSION

Subject Informations :

University        :  Anna University
Department     :  B.E. MECHANICAL ENGINEERING
Semester          :  06 th sem
Year                  :  03 rd year
Regulation       :  R2013
Subject Code   :  ME6604
Subject Name  :  GAS DYNAMICS AND JET PROPULSION

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ME6604 GAS DYNAMICS AND JET PROPULSION | Important  Questions

ME6604 GAS DYNAMICS AND JET PROPULSION – SYLLABUS – R- 2013

OBJECTIVES:

 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.

(Use of Standard Gas Tables permitted)

UNIT I BASIC CONCEPTS AND ISENTROPIC FLOWS

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

UNIT II FLOW THROUGH DUCTS

Flows through constant area ducts with heat transfer (Rayleigh flow) and Friction (Fanno flow) –
variation of flow properties.

UNIT III NORMAL AND OBLIQUE SHOCKS

Governing equations – Variation of flow parameters across the normal and oblique shocks – Prandtl – Meyer relations – Applications.

UNIT IV JET PROPULSION

Theory of jet propulsion – Thrust equation – Thrust power and propulsive efficiency – Operating
principle, cycle analysis and use of stagnation state performance of ram jet, turbojet, turbofan and
turbo prop engines.

UNIT V SPACE PROPULSION

Types of rocket engines – Propellants-feeding systems – Ignition and combustion – Theory of rocket
propulsion – Performance study – Staging – Terminal and characteristic velocity – Applications –
space flights.

TOTAL : 45 PERIODS

OUTCOMES:

 Upon completion of this course, the students can able to successfully apply gas dynamics
principles in the Jet and Space Propulsion

TEXT BOOKS:

1. Anderson, J.D., “Modern Compressible flow”, 3
rd Edition, McGraw Hill, 2003.
2. Yahya, S.M. “Fundamentals of Compressible Flow”, New Age International (P) Limited, New
Delhi, 1996.

REFERENCES:

1. Hill. P. and C. Peterson, “Mechanics and Thermodynamics of Propulsion”, Addison – Wesley
Publishing company, 1992.
2. Zucrow. N.J., “Aircraft and Missile Propulsion”, Vol.1 & II, John Wiley, 1975.
3. Zucrow. N.J., “Principles of Jet Propulsion and Gas Turbines”, John Wiley, New York, 1970.
4. Sutton. G.P., “Rocket Propulsion Elements”, John wiley, New York,1986,.
5. Shapiro. A.H.,” Dynamics and Thermodynamics of Compressible fluid Flow”, John wiley, New
York, 1953. 6. Ganesan. V., “Gas Turbines”, Tata McGraw Hill Publishing Co., New Delhi, 1999.
7. Somasundaram. PR.S.L., “Gas Dynamics and Jet Propulsions”, New Age International
Publishers, 1996.
8. Babu. V., “Fundamentals of Gas Dynamics”, ANE Books India, 2008.
9. Cohen. H., G.E.C. Rogers and Saravanamutto, “Gas Turbine Theory”, Longman Group Ltd.,

1980.

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