Related Questions
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4
In the aircraft propellers
A. The propulsive matter is caused to flow around the propelled body
B. Propulsive matter is ejected from within the propelled body
C. Its functioning does not depend on presence of air
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4
Isothermal compression efficiency can be attained by running the compressor
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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
The efficiency of jet engine is
B. Higher at high altitudes
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For minimum work in multistage compression, assuming same index of compression in all stages
A. Work done in first stage should be more
B. Work done in subsequent stages should increase
C. Work done in subsequent stages should decrease
D. Work done in all stages should be equal
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4
The compressor efficiency is the
A. Isothermal H.P/indicated H.R
B. Isothermal H.P./shaft H.R
C. Total output/air input
D. Compression work/motor input
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4
Reheating in a multistage expansion gas turbine __________ compressor work.
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A large clearance volume in a reciprocating compressor results in
A. Reduced volume flow rate
B. Increased volume flow rate
C. Lower suction pressure
D. Lower delivery pressure
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4
The capacity of compressor will be highest when its intake temperature is
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4
Gas turbine blades are given a rake
B. In the direction of motion of blades
C. Opposite to the direction of motion of blades
D. Depending on the velocity
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4
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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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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A compressor at high altitudes will require ________ power.
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In n₁ and n₂ are the indices of compression for the first and second stage of compression, then the ratio of workdone on the first and second stages (W₁/W₂) with perfect intercooling is given by
A. W₁/W₂ = n₂(n₁ - 1)/n₁(n₂ - 1)
B. W₁/W₂ = n₁(n₂ - 1)/n₂(n₁ - 1)
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4
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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4
Air-fuel ratio in a jet engine will be of the order of
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A closed cycle gas turbine gives ________ efficiency as compared to an open cycle gas turbine.
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In jet engines the products of combustion after passing through the gas turbine are discharged into
B. Back to the compressor
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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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4
When air is to be compressed at a high pressure, then it is advantageous to use
A. Single stage compression
B. Multistage compression without intercooling
C. Multistage compression with intercooling
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4
In air breathing jet engine, the jet is formed by expanding
A. Highly heated atmospheric air
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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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The volume of air delivered by the compressor is called
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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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4
During base load operation, the best method of controlling compressor is
B. Constant speed unloader
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A closed cycle gas turbine consists of a
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The pressure of air at the beginning of the compression stroke is ________ the atmospheric pressure.
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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
The ratio of outlet whirl velocity to blade velocity in case of centrifugal compressor is called
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For a two stage reciprocating compressor, compression from p₁ to p₃ is with perfect intercooling and no pressure losses. If compression in both the cylinders follows the same polytropic process and the atmospheric pressure is pa, then the intermediate pressure p₂ is given by