Work-done during adiabatic expansion is given by (where p1 v1, T1 = Pressure, volume and temperature for the initial condition of gas, p2, v2, T2 = Corresponding values for the final condition of gas, R = Gas constant, and γ = Ratio of specific heats)

Engineering Thermodynamics
Work-done during adiabatic expansion is given by (where p1 v1, T1 = Pressure, volume and temperature for the initial condition of gas, p2, v2, T2 = Corresponding values for the final condition of gas, R = Gas constant, and γ = Ratio of specific heats)

(p1 v1 - p2, v2)/(γ - 1)

[m R (T1 - T2)] /(γ - 1)

All of these

[m R T1/(γ - 1)][1 - (p2, v2 /p1 v1)]

(p1 v1 - p2, v2)/(γ - 1)

[m R (T1 - T2)] /(γ - 1)

All of these

[m R T1/(γ - 1)][1 - (p2, v2 /p1 v1)]

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Engineering Thermodynamics
In an irreversible process, there is a

Gain of heat

Loss of heat

No gain of heat

No loss of heat

Gain of heat

Loss of heat

No gain of heat

No loss of heat

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Engineering Thermodynamics
The general gas equation is (where p = Pressure, v = Volume, m = mass, T = Absolute temperature, and R = Gas constant)

pvm = C

pv = mRT

pv = RTm

pv = (RT)m

pvm = C

pv = mRT

pv = RTm

pv = (RT)m

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Engineering Thermodynamics
Temperature of a gas is produced due to

Repulsion of molecules

Its heating value

Surface tension of molecules

Kinetic energy of molecules

Repulsion of molecules

Its heating value

Surface tension of molecules

Kinetic energy of molecules

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Engineering Thermodynamics
Energy can neither be created nor destroyed, but it can be transformed from one form to another. This statement is known as

Zeroth law of thermodynamics

Second law of thermodynamics

First law of thermodynamics

Kinetic theory of gases

Zeroth law of thermodynamics

Second law of thermodynamics

First law of thermodynamics

Kinetic theory of gases

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Engineering Thermodynamics
Calorie is a measure of

Quantity of heat

Specific heat

Entropy

Thermal capacity

Quantity of heat

Specific heat

Entropy

Thermal capacity

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Engineering Thermodynamics

Engineering Thermodynamics Work-done during adiabatic expansion is given by (where p1 v1, T1 = Pressure, volume and temperature for the initial condition of gas, p2, v2, T2 = Corresponding values for the final condition of gas, R = Gas constant, and γ = Ratio of specific heats)

Engineering Thermodynamics In an irreversible process, there is a

Engineering Thermodynamics The general gas equation is (where p = Pressure, v = Volume, m = mass, T = Absolute temperature, and R = Gas constant)

Engineering Thermodynamics Temperature of a gas is produced due to

Engineering Thermodynamics Energy can neither be created nor destroyed, but it can be transformed from one form to another. This statement is known as

Engineering Thermodynamics Calorie is a measure of

Engineering Thermodynamics
Work-done during adiabatic expansion is given by (where p1 v1, T1 = Pressure, volume and temperature for the initial condition of gas, p2, v2, T2 = Corresponding values for the final condition of gas, R = Gas constant, and γ = Ratio of specific heats)

Engineering Thermodynamics
In an irreversible process, there is a

Engineering Thermodynamics
The general gas equation is (where p = Pressure, v = Volume, m = mass, T = Absolute temperature, and R = Gas constant)

Engineering Thermodynamics
Temperature of a gas is produced due to

Engineering Thermodynamics
Energy can neither be created nor destroyed, but it can be transformed from one form to another. This statement is known as

Engineering Thermodynamics
Calorie is a measure of