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4

Ratio of indicated H.P. and brake H.P. is known as

A. Mechanical efficiency

B. Volumetric efficiency

C. Isothermal efficiency

D. Adiabatic efficiency

Correct Answer :

A. Mechanical efficiency


Related Questions

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Mining industry usually employs following motive power

A. A.C. electric motor

B. Compressed air

C. Petrol engine

D. Diesel engine

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In a double acting compressor, the air is compressed

A. In one cylinder

B. In two cylinders

C. In a single cylinder on both sides of the piston

D. In two cylinders on both sides of the piston

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4

A turboprop is preferred to turbojet because

A. It has high propulsive efficiency at high speeds

B. It can fly at supersonic speeds

C. It can fly at high elevations

D. It has high power for take off

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4

Rotary compressors are suitable for

A. Large discharge at high pressure

B. Low discharge at high pressure

C. Large discharge at low pressure

D. Low discharge at low pressure

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A 3 m³/min compressor means that it

A. Compresses 3 m³/min of standard air

B. Compresses 3 m³/ min of free air

C. Delivers 3 m³/ min of compressed air

D. Delivers 3 m³/ min of compressed air at delivery pressure

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The ratio of the discharge pressure to the inlet pressure of air is called

A. Compression ratio

B. Expansion ratio

C. Compressor efficiency

D. Volumetric efficiency

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4

The work ratio of simple gas turbine cycle depends on

A. Pressure ratio

B. Maximum cycle temperature

C. Minimum cycle temperature

D. All of the above

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4

The ratio of outlet whirl velocity to blade velocity in case of centrifugal compressor is called

A. Slip factor

B. Velocity factor

C. Velocity coefficient

D. None of the above

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4

A jet engine has

A. No propeller

B. Propeller in front

C. Propeller at back

D. Propeller on the top

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4

Surging is the phenomenon of

A. Air stream blocking the passage

B. Motion of air at sonic velocity

C. Unsteady, periodic and reversed flow

D. Air stream not able to follow the blade contour

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4

Which of the following plants is smallest and lightest for generating a given amount of power?

A. Gas turbine plant

B. Petrol engine

C. Diesel engine

D. Solar plant

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4

Which is false statement about multistage compression?

A. Power consumption per unit of air delivered is low

B. Volumetric efficiency is high

C. It is best suited for compression ratios around 7:1

D. The moisture in air is condensed in the intercooler

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4

When the temperature of air leaving the intercooler, in a two stage compression with intercooler, is ________ the original atmospheric air temperature, then the intercooling is known as perfect or complete intercooling.

A. Equal to

B. Less than

C. More than

D. None of these

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4

Which of the following statement is correct as regard to centrifugal compressors?

A. The flow of air is parallel to the axis of the compressor

B. The static pressure of air in the impeller increases in order to provide centripetal force on the air

C. The impeller rotates at high speeds

D. The maximum efficiency is higher than multistage axial flow compressors

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4

The efficiency of a jet engine is higher at

A. Low speeds

B. High speeds

C. Low altitudes

D. High altitudes

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Which of the following statement is wrong?

A. In a two stage reciprocating air compressor with complete intercooling, maximum work is saved.

B. The minimum work required for a two stage reciprocating air compressor is double the work required for each stage.

C. The ratio of the volume of free air delivery per stroke to the swept volume of the piston is called volumetric efficiency.

D. None of the above

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4

For maximum work, the reheating should be done to an intermediate pressure of (Where p₁ = Maximum pressure, and p₂ = Minimum pressure)

A. (p₁ - p₂)/2

B. (p₁ + p₂)/2

C. p₁/p₂

D. p₁ p₂

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4

The volumetric efficiency of a compressor

A. Increases with decrease in compression ratio

B. Decreases with decrease in compression ratio

C. Increases with increase in compression ratio

D. Decreases with increase in compression ratio

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4

The workdone on a compressor will be minimum if air is taken from

A. The atmosphere

B. A source at 0°C

C. A source of low temperature air

D. A source of high temperature air

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4

The closed cycle in gas turbines

A. Provides greater flexibility

B. Provides lesser flexibility

C. In never used

D. Is used when gas is to be burnt

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It is not possible to use closed gas turbine cycle in aeronautical engines because

A. It is inefficient

B. It is bulky

C. It requires cooling water for its operation

D. None of the above

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A closed gas turbine in which fuel is burnt directly in the air is not possible because of

A. Paucity of O2

B. Increasing gas temperature

C. High specific volume

D. High friction losses

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4

The compressed air may be used

A. In gas turbine plants

B. For operating pneumatic drills

C. In starting and supercharging of I.C. engines

D. All of the above

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4

A rocket engine uses ________ for the combustion of its fuel.

A. Surrounding air

B. Compressed atmospheric air

C. Its own oxygen

D. None of these

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4

For perfect intercooling in a three stage compressor

A. p₂/p₁ = p₃/p₂ = p₄/p₃

B. p₃/p₁ = p₄/p₂

C. p₁ p₂ = p₃ p₄

D. p₁ p₃ = p₂ p₄

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Euler's equation is applicable for

A. Centrifugal compressor

B. Axial compressor

C. Pumps

D. All of the above

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4

Ramjet engine

A. Is self operating at zero flight speed

B. Is not self operating at zero flight speed

C. Requires no air for its operation

D. Produces a jet consisting of plasma

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4

In a high pressure compressor, the delivery pressure is

A. 1 to 5 bar

B. 5 to 8 bar

C. 8 to 10 bar

D. 10 to 15 bar

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In a jet engine, the air-fuel ratio is

A. 30 : 1

B. 40 : 1

C. 50 : 1

D. 60 : 1

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In multistage compressor, the isothermal compression is achieved by

A. Employing intercooler

B. By constantly cooling the cylinder

C. By running compressor at very slow speed

D. By insulating the cylinder