Compressors
1. 1 m of air at atmospheric condition weighs approximately
- 0.5 kg
- 1.0 kg
- 1.3 kg
- 2.2 kg
- 3.2 kg.
Correct answer: (C)
1.3 kg
2. A centrifugal compressor works on the principle of
- conversion of pressure energy into kinetic energy
- conversion of kinetic energy into presĀ¬sure energy
- centripetal action
- generating pressure directly
- combination of (a) and (d).
Correct answer: (B)
conversion of kinetic energy into presĀ¬sure energy
3. A closed gas turbine in which fuel is burnt directly in the air is not possible because of
- high pressure ratio
- increasing gas temperature
- high specific volume
- high friction losses
- paucity of 02.
Correct answer: (E)
paucity of 02.
4. A compressor at high altitude will draw
- more power
- less power
- same power
- more/less power depending on other factors
- none of the above.
Correct answer: (B)
less power
5. A gas turbine used in air craft should have
- high h.p. and low weight
- low weight and small frontal area
- small frontal area and high h.p.
- high speed and high h.p.
- all of the above.
Correct answer: (B)
low weight and small frontal area
6. A jet engine works on the principle of conservation of
- mass
- energy
- flow
- linear momentum
- angular momentum.
Correct answer: (D)
linear momentum
7. A rocket engine for the combustion of its fuel
- carries its own oxygen
- uses surrounding air
- uses compressed atmospheric air
- does not require oxygen
- depends on electrical energy supplied by solar cells.
Correct answer: (A)
carries its own oxygen
8. A rocket works with maximum overall efficiency when air craft velocity is equal to the
- jet velocity
- twice the jet velocity
- half the jet velocity
- average of the jet velocity
- no such co-relationship with jet velocity exists.
Correct answer: (C)
half the jet velocity
9. A simple turbo-jet engine is basically
- a propeller system
- gas-turbine engine equipped with a propulsive nozzle and diffuse*
- chemical rocket regine
- ram-jet enigne
- none of the above.
Correct answer: (B)
gas-turbine engine equipped with a propulsive nozzle and diffuse*
10. Actual compression curve is
- same as isothermal
- same as adiabatic
- better than isothermal and adiabatic
- in between isothermal and adiabatic
- none of the above.
Correct answer: (D)
in between isothermal and adiabatic