3rd Sem, AERO

Aero Engineering Thermodynamics Aero 3rd Sem Syllabus for BE 2017 Regulation Anna Univ

Aero Engineering Thermodynamics detail syllabus for Aeronautical Engineering (Aero), 2017 regulation is taken from Anna University official website and presented for students of Anna University. The details of the course are: course code (AE8301), Category (PC), Contact Periods/week (3), Teaching hours/week (3), Practical Hours/week (0). The total course credits are given in combined syllabus.

For all other aero 3rd sem syllabus for be 2017 regulation anna univ you can visit Aero 3rd Sem syllabus for BE 2017 regulation Anna Univ Subjects. The detail syllabus for aero engineering thermodynamics is as follows.”

Course Objective:

  • Aero Thermodynamics study includes quantitative analysis of machine and processes for transformation of energy and between work and heat.
  • Laws of thermodynamics would be able to quantify through measurement of related properties, to these energies and their interactions.
  • To develop basic concept of air cycle, gas turbine engines and heat transfer.

Unit I

For complete syllabus and results, class timetable and more pls download iStudy. Its a light weight, easy to use, no images, no pdfs platform to make students life easier.

Unit II

Second Law and Entropy
Second law of thermodynamics – Kelvin Planck and Clausius statements of second law. Reversibility and Irreversibility, Thermal reservoir, Carnot theorem. Carnot cycle, Reversed Carnot cycle, efficiency, COP, Thermodynamic temperature scale – Clausius inequality, Concept of entropy, Entropy change for various processes. Mixing of fluids.

Unit III

Air Standard Cycles
Otto, Diesel, Dual, Ericsson, Atkinson, Stirling and Brayton cycles – air standard efficiency – mean effective pressure.

Unit IV

For complete syllabus and results, class timetable and more pls download iStudy. Its a light weight, easy to use, no images, no pdfs platform to make students life easier.

Unit V

Basics of Propulsion and Heat Transfer
Classification of jet engines – basic jet propulsion arrangement – Engine station number, thrust equation – Specific thrust, SFC, TSFC, specific impulse, actual cycles, isentropic efficiencies of jet engine components, polytropic efficiency, conduction in parallel, radial and composite wall, basics of convective and radiation heat transfer.

Course Outcome:

  • Able to relate laws of thermodynamics to jet engine components.
  • Understands principle operation of piston engine and jet engines.
  • Able to identify efficient cycle of air and jet engines.
  • Capable to illustrate condition of working medium.
  • Eligible to recognize and calculate heat transfer in complex systems involving several heat transfer mechanisms.

Text Books:

  1. Nag.P.K., Engineering Thermodynamics, Tata McGraw-Hill, New Delhi, 2013.
  2. Rathakrishnan E., Fundamentals of Engineering Thermodynamics, Prentice-Hall India, 2005.
  3. Yunus A. Cengel and Michael A. Boles, Thermodynamics: An Engineering Approach McGraw-Hill Science/Engineering/Math; 7thedition 2010.

References:

  1. Arora C.P, Thermodynamics, Tata McGraw-Hill, New Delhi, 2003.
  2. Holman.J.P., Thermodynamics, 3rd Edition, McGraw-Hill, 2007.
  3. Merala C, Pother, Craig W, Somerton, Thermodynamics for Engineers, Schaum Outline Series,Tata McGraw-Hill, New Delhi, 2004.
  4. Ramalingam K.K. Thermodynamics, Sci-Tech Publications, 2006
  5. Venwylen and Sontag, Classical Thermodynamics, Wiley Eastern, 1987

For detail syllabus of all other subjects of BE Aero, 2017 regulation do visit Aero 3rd Sem syllabus for 2017 Regulation.

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