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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
rγ - 1
1 - rγ - 1
1 - (1/r) γ/γ - 1

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Engineering Thermodynamics
For a perfect gas, according to Boyle’s law (where P = Absolute pressure, V = Volume and T = Absolute temperature)

V/T = constant, if p is kept constant
P v = constant, if T is kept constant
T/P = constant, if v is kept constant
P/T = constant, if v is kept constant

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Engineering Thermodynamics
The natural solid fuel is

Anthracite coal
Wood
Pulverised coal
Coke

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Engineering Thermodynamics
The oxygen atom is ________ times heavier than the hydrogen atom.

2
16
8
32

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Engineering Thermodynamics
Otto cycle efficiency is higher than Diesel cycle efficiency for the same compression ratio and heat input because in Otto cycle

Heat rejection is lower
Expansion and compression are isentropic
Maximum temperature is higher
Combustion is at constant volume

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Engineering Thermodynamics
The gas turbine cycle with regenerator improves

Avoid pollution
None of these
Thermal efficiency
Work ratio

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