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Engineering Thermodynamics

Engineering Thermodynamics
The kinetic energy per kg molecule of any gas at absolute temperature T is equal to (where Ru = Universal gas constant)

3 Ru × T
1.5 Ru × T
Ru × T
2 Ru × T

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Engineering Thermodynamics
Specific heat of air at constant pressure is equal to

0.24
1
0.17
0.21

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Engineering Thermodynamics
The efficiency of Carnot cycle depends upon

Pressure ratio
Temperature limits
Cut-off ratio and compression ratio
Volume compression ratio

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Engineering Thermodynamics
Those substances which have so far not been resolved by any means into other substances of simpler form are called

Elements
Compounds
Atoms
Molecules

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Engineering Thermodynamics
Work done in an adiabatic process between a given pair of end states depends on

The end states only
Particular adiabatic process
The value of heat transferred
The value of index ‘n’

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Engineering Thermodynamics
The basis for measuring thermodynamic property of temperature is given by

First law of thermodynamics
Third law of thermodynamics
Zeroth law of thermodynamics
Second law of thermodynamics

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