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Engineering Thermodynamics

Engineering Thermodynamics
The work ratio of simple gas turbine cycle depends upon

Minimum cycle temperature
All of these
Maximum cycle temperature
Pressure ratio

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Engineering Thermodynamics
The ideal efficiency of a Brayton cycle without regeneration, with increase in pressure ratio will

Remain unchanged
Increase/decrease depending on application
Increase
Decrease

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Engineering Thermodynamics
One reversible heat engine operates between 1600 K and T2 K and another reversible heat engine operates between T2 K and 400 K. If both the engines have the same heat input and output, then temperature T2 is equal to

1400 K
1000 K
800 K
1200 K

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Engineering Thermodynamics
In a no flow reversible process for which p = (-3V + 15) × 105 N/m², V changes from 1 m3 to 2 m3. The work done will be about

10 × 10⁵ joules
1 × 10⁵ joules
100 × 10⁵ joules
10 × 10⁵ kilo joules

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Engineering Thermodynamics
The specific heat of air increases with increase in

Pressure
Both pressure and temperature
Variation of its constituents
Temperature

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Engineering Thermodynamics
The absolute zero pressure can be attained at a temperature of

None of these
273 K
-273°C
0°C

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MORE MCQ ON Engineering Thermodynamics

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