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ME8096 - Gas Dynamics and Jet Propulsion Syllabus (Elective I) Regulation 2017

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Code – ME8096, this article about B.E/B.Tech./B.Arch Mechanical Engineering Semester VI Gas Dynamics and Jet Propulsion Syllabus (Elective I) Syllabus. Students are requested to make notes or PDFs of the semester in Gas Dynamics and Jet Propulsion Syllabus for effective preparation from here. It will help you to understand what are the topics in the syllabus of Gas Dynamics and Jet Propulsion Syllabus.

And to make preparation strategies to score well in the examinations. Unit – wise detailed syllabus is given below in one place, in the following article ME8096 – Gas Dynamics and Jet Propulsion Syllabus. If the information helps you, kindly share it with your classmates.

If you want to know more about the syllabus of B.E Mechanical Engineering connected to an affiliated institution’s four-year undergraduate degree programme. We provide you with a detailed Year-wise, semester-wise, and Subject-wise syllabus in the following link B.E Mechanical Engineering Syllabus Anna University Regulation 2017.

Aim Of Concept:

  • 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)

ME8096 – Gas Dynamics and Jet Propulsion Syllabus (Elective I)

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: Flowthrough 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.

Text Books:

  1. Anderson, J.D., “Modern Compressible flow”, 3rd Edition, McGraw-Hill, 2012.
  2. Yahya, S.M. “Fundamentals of Compressible Flow”, New Age International (P) Limited, New Delhi, 2002.

References:

  1. Cohen. H., G.E.C. Rogers and Saravanamutto, “Gas Turbine Theory”, Longman Group Ltd.,1980
  2. Ganesan. V., “Gas Turbines”, Tata McGraw Hill Publishing Co., New Delhi, 2010.
  3. Shapiro. A.H.,” Dynamics and Thermodynamics of Compressible fluid Flow”, John Wiley, New York, 1953.
  4. Sutton. G.P., “Rocket Propulsion Elements”, John Wiley, New York,2010,.
  5. Zucrow. N.J., “Principles of Jet Propulsion and Gas Turbines”, John Wiley, NewYork, 1970.

If you want to check the syllabus of other branches provided by Anna University, Anna University syllabus Regulation 2017 will assist you in a clear path. Hope you find the required details.

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