Gas Dynamics and Jet Propulsion Mech (Sandwich) 7th Sem Syllabus for BE 2017 Regulation Anna Univ (Professional Elective II) detail syllabus for Mechanical Engineering (Sandwich) (Mech (Sandwich)), 2017 regulation is collected from the Anna Univ official website and presented for students of Anna University. The details of the course are: course code (ME8096), Category (PE), Contact Periods/week (3), Teaching hours/week (3), Practical Hours/week (0). The total course credits are given in combined syllabus.
For all other mech (sandwich) 7th sem syllabus for be 2017 regulation anna univ you can visit Mech (Sandwich) 7th Sem syllabus for BE 2017 regulation Anna Univ Subjects. For all other Professional Elective II subjects do refer to Professional Elective II. The detail syllabus for gas dynamics and jet propulsion is as follows.
Course 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.
(Use of Standard Gas Tables Permitted)
Unit I
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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
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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.
Course Outcome:
Upon the completion of this course the students will be able to
- CO1 Apply the concept of compressible flows in variable area ducts.
- CO2 Apply the concept of compressible flows in constant area ducts.
- CO3 examine the effect of compression and expansion waves in compressible flow.
- CO4 use the concept of gas dynamics in Jet Propulsion.
- CO5 apply the concept of gas dynamics in Space Propulsion.
Text Books:
- Anderson, J.D., “Modern Compressible flow”, 3rd Edition, McGraw Hill, 2012.
- Yahya, S.M. “Fundamentals of Compressible Flow”, New Age International (P) Limited, New Delhi, 2002.
References:
- Cohen. H., G.E.C. Rogers and Saravanamutto, “Gas Turbine Theory”, Longman Group Ltd.,1980
- Ganesan. V., “Gas Turbines”, Tata McGraw Hill Publishing Co., New Delhi, 2010.
- Shapiro. A.H.,” Dynamics and Thermodynamics of Compressible fluid Flow”, John wiley, New York, 1953.
- Sutton. G.P., “Rocket Propulsion Elements”, John wiley, New York,2010,.
- Zucrow. N.J., “Principles of Jet Propulsion and Gas Turbines”, John Wiley, New York, 1970.
For detail syllabus of all other subjects of BE Mech (Sandwich), 2017 regulation do visit Mech (Sandwich) 7th Sem syllabus for 2017 Regulation.
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