Q.1.

In a single stage impulse turbine, the velocity of steam approaching nozzles is negligible.

Q.2.

The ratio of the workdone on the blades per kg of steam to the total energy supplied per stage per kg of steam is called

Q.3.

The velocity of steam, in reaction turbines, is increased in the fixed blades as well as in moving blades.

Q.4.

The ratio of the isentropic heat drop to the heat supplied, is called

Q.5.

The pressure of steam __________ while flowing through a nozzle.

Q.6.

When the nozzle operates with the maximum mass flow, the nozzle is said to be

Q.7.

De-Laval turbine is a

Q.8.

Curtis turbine is a

Q.9.

The diagram efficiency is the ratio of

Q.10.

The critical pressure ratio for gases is

Q.11.

When the cross-section of a nozzle first increases from its entrance to throat, and then decreases from its throat to exit, it is not a convergent-divergent nozzle.

Q.12.

The process of maintaining the speed of the turbine constant for various load conditions, is known as

Q.13.

In a velocity compounded impulse turbine, when steam flows through the second row of moving blades,

Q.14.

The impulse turbine rotor efficiency will have a maximum value of 0.5 cos2 α, where α is the nozzle exit flow angle, if the

Q.15.

The reheat factor depends upon

Q.16.

In order to reduce the rotor speed of an impulse turbine, the method employed is

Q.17.

The velocity of steam at throat of the nozzle is __________ the velocity of sound.

Q.18.

The critical pressure ratio for initially dry saturated steam is

Q.19.

The Rankine efficiency depends upon total useful heat drop and total isentropic heat drop.

Q.20.

The efficiency of a pressure-velocity compounded impulse turbine is __________ as compared to pressure compounded impulse turbine.

Q.21.

The efficiency ratio is the ratio of total useful heat drop to the total isentropic heat drop.

Q.22.

Reheating of steam in a turbine

Q.23.

The ratio of the energy supplied to the blades per kg of steam to the total energy supplied per stage per kg of steam is called mechanical efficiency.

Q.24.

When the cross-section of a nozzle increases continuously from entrance to exit, it is called a

Q.25.

In an impulse turbine

Q.26.

The nozzle efficiency is the ratio of

Q.27.

The discharge through a nozzle is maximum for a certain value of exit pressure. This pressure is known as critical pressure.

Q.28.

Blading efficiency is also known as

Q.29.

The effect of supersaturation is that the

Q.30.

The purpose of governing in steam turbines is to