Q.1

The ratio of the indicated power to the shaft power or brake power of the motor or engine required to drive the compressor, is called

  • compressor efficiency
  • volumetric efficiency
  • isothermal efficiency
  • mechanical efficiency
Q.2

The efficiency of a jet engine is higher at

  • low speeds
  • high speeds
  • low altitudes
  • high altitudes
Q.3

The capacity of a compressor is expressed in

  • kg/m2
  • kg/m3
  • m3/min
  • m3/kg
Q.4

The increase in pressure in a roots blower is entirely due to back flow of air.

  • Agree
  • Disagree
Q.5

A large clearance Volume in a reciprocating compressor results in

  • reduced volume flow rate
  • increased volume flow rate
  • lower suction pressure
  • lower delivery pressure
Q.6

The rotary compressors are suitable for large discharge of air at low pressure.

  • True
  • False
Q.7

Intercooling in multi-stage compressors is done

  • to cool the air during compression
  • to cool the air at delivery
  • to enable compression in two stages
  • to minimise the work of compression
Q.8

The type of rotary compressor used in aeroplanes, is of

  • centrifugal type
  • axial flow type
  • radial flow type
  • none of these
Q.9

A closed cycle gas turbine gives __________ efficiency as compared to an open cycle gas turbine.

  • same
  • lower
  • higher
Q.10

The stagnation pressure rise in a centrifugal compressor takes place

  • in the diffuser only
  • in the impeller only
  • in the diffuser and impeller
  • in the inlet guide vanes only
Q.11

For a two stage reciprocating compressor, compression from p1 to p3 is with perfect intercooling and no pressure losses. If compression in both the cylinders follows the same polytropic process and the atmospheric pressure is pa, then the intermediate pressure p2 is given by

  • p2 = (p1 + p3)/2
  • p2 = p1.p3
  • P2 = Pa x p3/p1
  • p2 = pa p3/p1
Q.12

An axial compressor gives optimum performance at high speeds and large volume flows.

  • Agree
  • Disagree
Q.13

Gas turbine as compared to steam turbine

  • requires less space for installation
  • has compressor and combustion chamber
  • has less efficiency
  • all of these
Q.14

The total heat rejected in a reciprocating air compressor is equal to the sum of the heat rejected during polytropic compression per kg of air and heat rejected in the intercooler per kg of air.

  • True
  • False
Q.15

The ratio of workdone per cycle to the stroke volume of the compressor is known as

  • compressor capacity
  • compression ratio
  • compressor efficiency
  • mean effective pressure
Q.16

In a reciprocating air compressor, the compression work per kg of air

  • increases as clearance volume increases
  • decreases as clearance volume increases
  • is independent of clearance volume
  • increases as clearance volume decreases
Q.17

The degree of reaction in an axial flow compressor is defined as the ratio of static enthalpy rise in the

  • rotor to static enthalpy rise in the stator
  • stator to static enthalpy rise in the rotor
  • rotor to static enthalpy rise in the stage
  • stator to static enthalpy rise in the stage
Q.18

Intercooling in gas turbines

  • decreases net output but increases thermal efficiency
  • increases net output but decreases thermal efficiency
  • decreases net output and thermal efficiency both
  • increases net output and thermal efficiency both
Q.19

In a jet propulsion

  • the propulsive matter is ejected from within the propelled body
  • the propulsive matter is caused to flow around the propelled body
  • its functioning does not depend upon presence of air
  • none of the above
Q.20

The clearance volume in the compressor is kept minimum because it effects on volumetric efficiency.

  • Correct
  • Incorrect
Q.21

When the temperature of air leaving the intercooler, in a two stage compression with intercooler, is __________ the original atmospheric air temperature, then the intercooling is known as perfect or complete intercooling.

  • equal to
  • less than
  • more than
Q.22

An open cycle gas turbine works on the same cycle as that of a closed cycle gas turbine.

  • Yes
  • No
Q.23

The inlet pressure is always __________ the discharge pressure.

  • equal to
  • less than
  • more than
Q.24

The temperature of air at the beginning of the compression stroke is __________ the atmospheric temperature.

  • equal to
  • less than
  • more than
Q.25

Free air is the air at atmospheric conditions at any specific location.

  • True
  • False
Q.26

The axial flow compressor is preferred in air-craft gas turbines because of

  • low frontal area
  • higher thrust
  • high pressure rise
  • none of these
Q.27

In a compressed air system, the temperature of air discharged from the air motor is __________ than the initial compressor intake temperature.

  • more
  • less
Q.28

The performance of air compressor at high altitudes will be __________ as compared to that at sea level.

  • same
  • lower
  • higher
Q.29

The compressor efficiency is defined as the ratio of volume of free air delivery per stroke to the swept volume of the piston.

  • Correct
  • Incorrect
Q.30

A gas turbine used in air-craft should have low weight and small frontal area.

  • Correct
  • Incorrect
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