Compressors

1. 1 m of air at atmospheric condition weighs approximately

  1. 0.5 kg
  2. 1.0 kg
  3. 1.3 kg
  4. 2.2 kg
  5. 3.2 kg.

Correct answer: (C)
1.3 kg

2. A centrifugal compressor works on the principle of

  1. conversion of pressure energy into kinetic energy
  2. conversion of kinetic energy into presĀ¬sure energy
  3. centripetal action
  4. generating pressure directly
  5. 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

  1. high pressure ratio
  2. increasing gas temperature
  3. high specific volume
  4. high friction losses
  5. paucity of 02.

Correct answer: (E)
paucity of 02.

4. A compressor at high altitude will draw

  1. more power
  2. less power
  3. same power
  4. more/less power depending on other factors
  5. none of the above.

Correct answer: (B)
less power

5. A gas turbine used in air craft should have

  1. high h.p. and low weight
  2. low weight and small frontal area
  3. small frontal area and high h.p.
  4. high speed and high h.p.
  5. all of the above.

Correct answer: (B)
low weight and small frontal area

6. A jet engine works on the principle of conservation of

  1. mass
  2. energy
  3. flow
  4. linear momentum
  5. angular momentum.

Correct answer: (D)
linear momentum

7. A rocket engine for the combustion of its fuel

  1. carries its own oxygen
  2. uses surrounding air
  3. uses compressed atmospheric air
  4. does not require oxygen
  5. 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

  1. jet velocity
  2. twice the jet velocity
  3. half the jet velocity
  4. average of the jet velocity
  5. no such co-relationship with jet velocity exists.

Correct answer: (C)
half the jet velocity

9. A simple turbo-jet engine is basically

  1. a propeller system
  2. gas-turbine engine equipped with a propulsive nozzle and diffuse*
  3. chemical rocket regine
  4. ram-jet enigne
  5. none of the above.

Correct answer: (B)
gas-turbine engine equipped with a propulsive nozzle and diffuse*

10. Actual compression curve is

  1. same as isothermal
  2. same as adiabatic
  3. better than isothermal and adiabatic
  4. in between isothermal and adiabatic
  5. none of the above.

Correct answer: (D)
in between isothermal and adiabatic

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