AERONAUTICAL ENGINEERING
UNIT-I BASIC CONCEPTS
AND FIRST LAW
Concept of
continuum, macroscopic approach, thermodynamic systems – closed, open and
isolated. Property, state, path and process, quasi-static process, work, modes
of work, Zeroth law of thermodynamics- concept of temperature and heat,
internal energy, specific heat capacities, enthalpy - concept of ideal and real
gases. First law of thermodynamics - applications to closed and open systems -
steady flow processes with reference to various thermal equipment’s.
UNIT-II SECOND LAW AND ENTROPY
Second law of
thermodynamics – kelvin Planck and Clausius statements of second law.
Reversibility and irreversibility - Carnot theorem. Carnot cycle, reversed
Carnot cycle, efficiency, COP - thermodynamic temperature scale - Clausius
inequality, concept of entropy, entropy of ideal gas, principle of increase of
entropy.
UNIT III AIR STANDARD CYCLES
Otto, Diesel, Dual combustion and Brayton combustion cycles – Air standard efficiency - Mean effective pressure – Actual and theoretical PV, TS diagrams of two stroke and four stroke IC Engines.
UNIT IV REFRIGERATION AND AIR CONDITIONING
Principles of refrigeration, Air
conditioning - Heat pumps - Vapour compression - Vapour absorption types -
Coefficient of performance, Properties of refrigerants.
UNIT V AIR COMPRESSORS
Classification and working principle of compressors (Descriptive
Treatment). Isothermal and Isentropic efficiency of air compressors.
0 Comments
Post a Comment