Online Mechanical Engineering Test - Steam Nozzles and Turbines Test

Instruction:

  • This is a FREE online test. Beware of scammers who ask for money to attend this test.
  • Total number of questions: 20.
  • Time allotted: 30 minutes.
  • Each question carries 1 mark; there are no negative marks.
  • DO NOT refresh the page.
  • All the best!

Marks : 2/20


Total number of questions
20
Number of answered questions
0
Number of unanswered questions
20
Test Review : View answers and explanation for this test.

1.
The steam enters the nozzle at a
high pressure and a low velocity
high pressure and a high velocity
low pressure and a low velocity
low pressure and a high velocity
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2.
In a De-Laval nozzle expanding superheated steam from 10 bar to 0.1 bar, the pressure at the minimum cross-section (i. e. pressure at throat, p2) will be
3.3 bar
5.46 bar
8.2 bar
9.9 bar
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3.
The action of steam in a steam turbine is
static
dynamic
static and dynamic
neither static nor dynamic
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4.
De-Laval turbine is a
single rotor impulse turbine
multi-rotor impulse turbine
impulse reaction turbine
none of these
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5.
Steam turbines are used for
large marine propulsion
electric power generation
direct drive of fans, compressors, pumps
all of these
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6.
A steam nozzle converts
heat energy of steam into kinetic energy
kinetic energy into heat energy of steam
heat energy of steam into potential energy
potential energy into heat energy of steam
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7.
The flow of steam is super-sonic
at the entrance to the nozzle
at the throat of the nozzle
in the convergent portion of the nozzle
in the divergent portion of the nozzle
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8.
The velocity of steam at throat of the nozzle is __________ the velocity of sound.
equal to
less than
more than
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9.
In an impulse turbine
the steam is expanded in nozzles only and there is a pressure drop and heat drop
the steam is expanded both in fixed and moving blades continuously
the steam is expanded in moving blades only
the pressure and temperature of steam remains constant
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10.
In a reaction turbine
the steam is allowed to expand in the nozzle, where it gives a high velocity before it enters the moving blades
the expansion of steam takes place partly in the fixed blades and partly in the moving blades
the steam is expanded from a high pressure to a condenser pressure in one or more nozzles
the pressure and temperature of steam remains constant
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11.
Rateau turbine is
simple reaction turbine
velocity compounded turbine
pressure compounded turbine
pressure-velocity compounded turbine
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12.
Curtis turbine is a
simple reaction turbine
velocity compounded turbine
pressure compounded turbine
pressure-velocity compounded turbine
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13.
The ratio of the isentropic heat drop to the heat supplied, is called
reheat factor
stage efficiency
internal efficiency
Rankine efficiency
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14.
The ratio of the work delivered at the turbine shaft to the heat supplied is called overall thermal efficiency of turbine.
True
False
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15.
A nozzle is said to be a convergent-divergent nozzle, when the cross-section of a nozzle first decreases from its entrance to throat and then increases from its throat to exit.
True
False
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16.
When the cross-section of a nozzle __________ continuously from entrance to exit, it is called a convergent nozzle.
increases
decreases
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17.
The friction present between the steam and the nozzle surfaces reduces the heat drop by
10 to 15 percent
15 to 25 percent
25 to 40 percent
40 to 60 percent
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18.
Steam turbines may be classified according to
direction of steam flow
number of stages
mode of steam action
all of these
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19.
In turbines, the fluid undergoes a continuous steady flow process and the speed of flow is
low
very low
high
very high
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20.
The blade friction in the impulse turbine reduces the velocity of steam by __________ while it passes over the blades.
10 to 15%
15 to 20%
20 to 30%
30 to 40%
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*** END OF THE TEST ***
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