Latent heat of vaporisation
Chemical potential
Molal boiling point
Heat capacity
Ideal compression of air
Free expansion of an ideal gas
Adiabatic expansion of steam in a turbine
Adiabatic compression of a perfect gas
Single phase fluid of varying composition
Single phase fluid of constant composition
Open as well as closed systems
Both (B) and (C)
Molecular size
Volume
Pressure
Temperature
By throttling
By expansion in an engine
At constant pressure
None of these
Zero
+ve
-ve
Dependent on the path
349
651
667
1000
Maxwell's equation
Clausius-Clapeyron Equation
Van Laar equation
Nernst Heat Theorem
Increases, for an exothermic reaction
Decreases, for an exothermic reaction
Increases, for an endothermic reaction
None of these
Pressure to critical pressure
Critical pressure to pressure
Pressure to pseudocritical pressure
Pseudocritical pressure to pressure
Ideal
Real
Isotonic
None of these
Zero
Unity
Infinity
None of these
The values of (∂P/∂V)T and (∂2P/∂V2)T are zero for a real gas at its critical point
Heat transferred is equal to the change in the enthalpy of the system, for a constant pressure, non-flow, mechanically reversible process
Thermal efficiency of a Carnot engine depends upon the properties of the working fluid besides the source & sink temperatures
During a reversible adiabatic process, the entropy of a substance remains constant
Not liquify (barring exceptions)
Immediately liquify
Never liquify however high the pressure may be
None of these
Ethyl chloride or methyl chloride
Freon-12
Propane
NH3 or CO2
dE = CpdT
dE = CvdT
dQ = dE + pdV
dW = pdV
Heating takes place
Cooling takes place
Pressure is constant
Temperature is constant
Minimum number of degree of freedom of a system is zero
Degree of freedom of a system containing a gaseous mixture of helium, carbon dioxide and hydrogen is 4
For a two phase system in equilibrium made up of four non-reacting chemical species, the number of degrees of freedom is 4
Enthalpy and internal energy change is zero during phase change processes like melting, vaporisation and sublimation
Eutectic
Triple
Plait
Critical
Increased COP
Same COP
Decreased COP
Increased or decreased COP; depending upon the type of refrigerant
5 & 3
3.987 & 1.987
1.987 & 0.66
0.66 & 1.987
Adiabatic
Isometric
Isentropic
Isothermal
Equal to its density
The reciprocal of its density
Proportional to pressure
None of these
Critical temperature
Melting point
Freezing point
Both (B) and (C)
Solution
Vaporisation
Formation
Sublimation
Isochoric
Isobaric
Adiabatic
Isothermal
x
x + 1
x + 2
x + 3
Entropy
Temperature
Enthalpy
Pressure
Gibbs-Duhem
Gibbs-Helmholtz
Maxwell's
None of these
Isothermally
Isobarically
Adiabatically
None of these