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Higher Study | Mechanical Engineering | Compressors

The compression ratio for the compressor is always _________ unity.
The hottest point in a gas turbine is
Temperature of gases at end of compression as compared to exhaust gases in a gas turbine is
The maximum temperature in a gas turbine is
In a jet propulsion
The fuel consumption in gas turbines is accounted for by
The indicated work per unit mass of air delivered is
Which of the following plants is smallest and lightest for generating a given amount of power?
In jet engines, for the efficient production of large power, fuel is burnt in an atmosphere of
Gas turbine blades are given a rake
Water gas is produced by
In open cycle turbojet engines used in military aircraft, reheating the exhaust gas from the turbine by burning, more fuel is used to increase the
A compressor at high altitudes will require ________ power.
In a jet propulsion unit, the products of combustion after passing through the gas turbine are discharged into
In jet engines the products of combustion after passing through the gas turbine are discharged into
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