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

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Engineering Thermodynamics
The mass of excess air supplied is equal to

(23/100) × Mass of excess oxygen
(100/23) × Mass of excess oxygen
(100/23) × Mass of excess carbon
(23/100) × Mass of excess carbon

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Engineering Thermodynamics
In an isothermal process, the internal energy of gas molecules

Increases
Decreases
Remain constant
May increase/decrease depending on the properties of gas

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Engineering Thermodynamics
In S. I. units, the value of the universal gas constant is

8314 J/kg mole-K
83.14 J/kg mole-K
831.4 J/kg mole-K
8.314 J/kg mole-K

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Engineering Thermodynamics
A path 1-2-3 is given. A system absorbs 100 kJ as heat and does 60 kJ of work while along the path 1-4-3, it does 20 kJ of work. The heat absorbed during the cycle 1-4-3 is

+60 kJ
-40 kJ
-80 kJ
-140 kJ

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Engineering Thermodynamics
Which of the following is a reversible non-flow process?

Isobaric process
Isochoric process
Hyperbolic process
All of these

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MORE MCQ ON Engineering Thermodynamics

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