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Engineering Thermodynamics

Engineering Thermodynamics
The thermal efficiency of an ideal gas turbine plant is given by (where r = Pressure ratio)

1 - (1/r) γ - 1/ γ
1 - (1/r) γ/γ - 1
1 - rγ - 1
rγ - 1

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Engineering Thermodynamics
Universal gas constant is defined as equal to product of the molecular weight of the gas and

Specific heat at constant volume
Ratio of two specific heats
Gas constant
Specific heat at constant pressure

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Engineering Thermodynamics
The cycle in which heat is supplied at constant volume and rejected at constant pressure is known as

Dual combustion cycle
Diesel cycle
Rankine cycle
Atkinson cycle

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Engineering Thermodynamics
The unit of temperature in S.I. units is

Celsius
Fahrenheit
Kelvin
Centigrade

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Engineering Thermodynamics
An open cycle gas turbine works on

Carnot cycle
Otto cycle
Joule's cycle
Stirling cycle

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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

First law of thermodynamics
Kinetic theory of gases
Zeroth law of thermodynamics
Second law of thermodynamics

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