Two different gases behave similarly, if their reduced properties (i.e. P, V and T) are same
The surface of separation (i. e. the meniscus) between liquid and vapour phase disappears at the critical temperature
No gas can be liquefied above the critical temperature, howsoever high the pressure may be.
The molar heat of energy of gas at constant volume should be nearly constant (about 3 calories)
A. Two different gases behave similarly, if their reduced properties (i.e. P, V and T) are same
Reversible isothermal volume change
Heating of a substance
Cooling of a substance
Simultaneous heating and expansion of an ideal gas
Isothermal
Isentropic
Isobaric
Adiabatic
Water
Air
Evaporative
Gas
CV
Enthalpy change
Free energy change
None of these
Sublimation
Fusion
Transition
Vaporisation
Zero
Positive
Negative
None of these
The statement as per Gibbs-Helmholtz
Called Lewis-Randall rule
Henry's law
None of these
A refrigeration cycle violates the second law of thermodynamics
Refrigeration cycle is normally represented by a temperature vs. entropy plot
In a refrigerator, work required decreases as the temperature of the refrigerator and the temperature at which heat is rejected increases
One ton of refrigeration is equivalent to the rate of heat absorption equal to 3.53 kW
Constant volume
Polytropic
Adiabatic
Constant pressure
1.987 cal/gm mole °K
1.987 BTU/lb. mole °R
Both (A) and (B)
Neither (A) nor (B)
Increases
Decreases
Remain constant
Increases linearly
Increases
Decreases
Remains unchanged
May increase or decrease; depends on the substance
Indeterminate
Zero
Negative
None of these
Tds = dE + dW
dE - dW = Tds
dW - dE = Tds
Tds - dW + dE >0
Isothermal
Adiabatic
Isentropic
Polytropic
Mass
Energy
Momentum
None of these
(T2 - T1)/T2
(T2 - T1)/T1
(T1 - T2)/T2
(T1 - T2)/T1
35 K
174 K
274 K
154 K
(∂T/∂V)S = - (∂P/∂S)V
(∂S/∂P)T = - (∂V/∂T)P
(∂V/∂S)P = (∂T/∂P)S
(∂S/∂V)T = (∂P/∂T)V
Does not need the addition of external work for its functioning
Transfers heat from high temperature to low temperature
Accomplishes the reverse effect of the heat engine
None of these
Steam engine
Carnot engine
Diesel engine
Otto engine
Chemical potential
Fugacity
Both (A) and (B)
Neither (A) nor (B)
Sublimation
Vaporisation
Melting
Either (A), (B) or (C)
(∂P/∂V)S = (∂P/∂V)T
(∂P/∂V)S = [(∂P/∂V)T]Y
(∂P/∂V)S = y(∂P/∂V)T
(∂P/∂V)S = 1/y(∂P/∂V)T
0°C
273°C
100°C
-273°C
Pressure
Temperature
Both (A) & (B)
Neither (A) nor (B)
RT d ln P
R d ln P
R d ln f
None of these
No heat and mass transfer
No mass transfer but heat transfer
Mass and energy transfer
None of these
T = [RT/(V- b)] - [a/√T. V(V + b)]
PV/RT = 1 + (B/V) + (C/V2) + ……
n1u2 + μ2μ1 = 0
None of these
Temperature vs. enthalpy
Temperature vs. enthalpy
Entropy vs. enthalpy
Temperature vs. internal energy