Related Questions
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The volume of air sucked by the compressor during its suction stroke is called
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The work ratio of a gas turbine plant is defined as the ratio of
A. Net work output and heat supplied
B. Net work output and work done by turbine
C. Actual heat drop and isentropic heat drop
D. Net work output and isentropic heat drop
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4
Out of the following, from where you will prefer to take intake for air compressor
A. From an air conditioned room maintained at 20°C
B. From outside atmosphere at 1°C
D. From a side where cooling tower is located nearby
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4
Isothermal compression efficiency can be attained by running the compressor
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A compressor mostly used for supercharging of I.C. engines is
A. Radial flow compressor
D. Reciprocating compressor
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A machine used to raise the pressure of air is called
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Temperature of gases at end of compression as compared to exhaust gases in a gas turbine is
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If the flow of air through the compressor is perpendicular to its axis, then it is a
A. Reciprocating compressor
B. Centrifugal compressor
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Propulsive efficiency is defined as ratio of
A. Thrust power and fuel energy
B. Engine output and propulsive power
C. Propulsive power and fuel input
D. Thrust power and propulsive power
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4
Work ratio of a gas turbine plant is ratio of
A. Net work output and work done by turbine
B. Net work output and heat supplied
C. Work done by turbine and heat supplied
D. Work done by turbine and net work output
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In an axial flow compressor, the ratio of pressure in the rotor blades to the pressure rise in the compressor in one stage is known as
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The volumetric efficiency of a compressor falls roughly as follows for every 100 m increase in elevation
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In a single acting reciprocating air compressor, without clearance, the compression of air may be
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A closed cycle gas turbine consists of a
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The material commonly used for air craft gas turbine is
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The thrust of a jet propulsion power unit can be increased by
A. Injecting water into the compressor
B. Burning fuel after gas turbine
C. Injecting ammonia into the combustion chamber
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The degree of reaction of an axial flow turbine is the ratio of isentropic temperature drop in a blade row to the
A. Adiabatic temperature drop in the stage
B. Total temperature drop
C. Total temperature drop in the stage
D. Total adiabatic temperature drop
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The compressor capacity with decrease in suction temperature
D. May increase or decrease depending on compressor capacity
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The capacity of compressor will be highest when its intake temperature is
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If the clearance ratio for a reciprocating air compressor is 'K', then its volumetric efficiency is given by
C. 1 - k + k (p₁/p₂) n- 1/n
D. 1 + k - k (p₂/p₁) n-1/n
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In a centrifugal compressor, an increase in speed at a given pressure ratio causes
C. Increase in efficiency
D. Increase in flow and decrease in efficiency
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The degree of reaction is usually kept ________ for all types of axial flow compressors.
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A closed cycle gas turbine gives ________ efficiency as compared to an open cycle gas turbine.
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The volumetric efficiency of a compressor falls roughly as follows for every 5°C increase in atmospheric temperature
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Propulsion efficiency of the following order is obtained in practice
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In a single stage, single acting reciprocating air compressor, without clearance, the workdone on the air during isentropic compression is ________ the heat required to raise the temperature of air from T₁ to T₂ at a constant pressure.
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The overall thermal efficiency of an ideal gas turbine plant is (where r = Pressure ratio)
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If p₁, is the pressure of air entering the L.P. cylinder and p₂ is the pressure of air leaving the L.P. cylinder (or intercooler pressure), then the ratio of cylinder diameters for a single acting, two stage reciprocating air compressor with complete intercooling is given by (where D₁ = Dia. of L.P. cylinder, and D₂ = Dia. of H.P. cylinder)
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The clearance volume of the air compressor is kept minimum because
A. It allows maximum compression to be achieved
B. It greatly affects volumetric efficiency
C. It results in minimum work
D. It permits isothermal compression
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A rocket engine for the combustion of its fuel
A. Carries its own oxygen
C. Uses compressed atmospheric air
D. Does not require oxygen