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Steam Nozzles and Turbines - Section 1

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  • Steam Nozzles and Turbines - Section 1
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Steam Nozzles and Turbines - Section 1

1. 

The velocity of steam leaving the nozzle (V) is given by (where K = Nozzle coefficient or nozzle efficiency, and hd = Enthalpy or heat drop during expansion of steam in a nozzle)

A. V = 44.72 hd
B. V = 44.72 K
C. V = 44.72
D. V = 44.72 K hd

Answer: Option C

Explanation:

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2. 

The rate of discharge through the nozzle __________ when the exit pressure is gradually reduced.

A. remains same
B. decreases
C. increases

Answer: Option C

Explanation:

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3. 

The discharge of steam in a convergent-divergent nozzle __________ after the throat (i.e. in the divergent portion of the nozzle)

A. remains constant
B. decreases
C. increases

Answer: Option A

Explanation:

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4. 

The pressure at which the steam leaves the nozzle is known as back pressure.

A. Correct
B. Incorrect

Answer: Option A

Explanation:

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5. 

The ratio of total useful heat drop to the total isentropic heat drop, is called

A. stage efficiency
B. internal efficiency
C. Rankine efficiency
D. none of these

Answer: Option B

Explanation:

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6. 

The flow through a nozzle is regarded as

A. constant volume flow
B. constant pressure flow
C. isothermal flow
D. isentropic flow

Answer: Option D

Explanation:

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7. 

A turbine is said to have an axial discharge when the steam leaves the blade tip at __________ to the direction of the blade motion.

A. 60°
B. 90°
C. 180°
D. 270°

Answer: Option B

Explanation:

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8. 

A nozzle is said to be a convergent nozzle

A. when the cross-section of the nozzle increases continuously from entrance to exit
B. when the cross-section of the nozzle decreases continuously from entrance to exit
C. when the cross-section of the nozzle first decreases from entrance to throat and then increases from its throat to exit
D. none of the above

Answer: Option B

Explanation:

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