Syllabus

JNTUH B.Tech 2016-2017 (R16) Detailed Syllabus Air Breathing Propulsion

Air Breathing Propulsion Detailed Syllabus for B.Tech third year first sem is covered here. This gives the details about credits, number of hours and other details along with reference books for the course.

The detailed syllabus for Air Breathing Propulsion B.Tech 2016-2017 (R16) third year first sem is as follows.

B.Tech. III Year I Sem.            L/T/P/C
Course Code:AE502PC              4/0/0/4

UNIT – I: Gas Turbine Theories: Impulse and reaction balding of gas turbines, Velocity triangles and power output, Elementary theory, Vortex theory. Choice of blade profile, pitch and chord, Estimation of stage performance. Design Consilretions: Limiting factors in gas turbine design, Overall turbine performance. Methods of blade cooling, matching of turbine and compressor, Numerical problems.

UNIT – II:  Thrust Control: Thrust Augmentation through after burning, thrust vector control methods. RAMJET Propulsion: Operating principle Subcritical, critical and supercritical operation. Combustion in ramjet engine, Ramjet performance, Sample ramjet design calculations. Introduction to SCRAMJET, Preliminary concepts in supersonic combustion, Integral ram, Rocket, Numerical problems.

UNIT – III:  Chemical Rockets: Solid Propellant: Solid propellant rockets, Selection criteria of solid
propellants, important hardware components of solid rockets, Propellant grain design  considerations.  Liquid Propellant: Liquid propellant rockets, cooling in liquid rockets. Limitations of hybrid rockets, Relative advantages of liquid rockets over solid rockets.

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TEXT BOOKS:

  • Sutton G. P. (2010), Rocket Propulsion Elements, 8th edition, John Wiley & Sons Inc, USA.
  • Philipa Hill, Carl Peterson (2010), Mechanics and Thermodynamics of Propulsion, 2nd edition, Addison Wesley Longman Inc, USA.

REFERENCE BOOKS:

  • Oates G. C (1986), Aero Thermodyanamics of Aircraft Engine Components, AIAA Educational Series, USA.
  • Rolls- Royce (2005), Jet Engine, 6th edition, Rolls – Royce Ltd, USA.
  • Ganesan V (2010), Gas Turbines, Tata McGraw- Hill, New Delhi.
  • S. M. Yahya(2010), Fundamentals of Compressible Flow with Aircraft and Rocket propulsion, 4th Edition, New Age International Publications, New Delhi.

For all other B.Tech 3rd Year 1st Sem syllabus go to JNTUH B.Tech Aeronautical Engineering 3rd Year 1st Sem Course Structure for (R16) Batch.

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