AE8301-AERO ENGINEERING THERMODYNAMICS Syllabus 2017 Regulation
AE8301-AERO ENGINEERING THERMODYNAMICS Syllabus 2017 Regulation
AE8301 AERO ENGINEERING THERMODYNAMICS L T P C
3 0 0 3
OBJECTIVES:
- 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 FUNDAMENTAL CONCEPT AND FIRST LAW 9
Concept of continuum, macroscopic approach, thermodynamic systems – closed, open and isolated. Property, state, path and process, quasi-static process, work, internal energy, enthalpy, specific heat capacities and heat transfer, SFEE, application of SFEE to jet engine components, First law of thermodynamics, relation between pressure, volume and temperature for various processes, Zeroth law of thermodynamics.
UNIT II SECOND LAW AND ENTROPY 9
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 8
Otto, Diesel, Dual, Ericsson, Atkinson, Stirling and Brayton cycles – air standard efficiency – mean effective pressure.
UNIT IV FUNDAMENTALS OF VAPOUR POWER CYCLES 9
Properties of pure substances – solid, liquid and vapour phases, phase rule, p-v, p-T, T-v, T-s, h-s diagrams, p-v-T surfaces, thermodynamic properties of steam – calculations of work done and heat transfer in non-flow and flow processes – standard Rankine cycle, Reheat and Regeneration cycle. Heat rate, Specific steam consumption, Tonne of refrigeration.
UNIT V BASICS OF PROPULSION AND HEAT TRANSFER 10
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.
TOTAL: 45 PERIODS
OUTCOMES
- 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:
- Nag.P.K. “Engineering Thermodynamics” Tata McGraw-Hill, New Delhi, 2013.
- Rathakrishnan E., “Fundamentals of Engineering Thermodynamics”, Prentice-Hall India, 2005.
- 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
