Question Category: Mechanical Engineering

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The combustion efficiency of a gas turbine using perfect combustion chamber is of the order of
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It is not possible to use closed gas turbine cycle in aeronautical engines because
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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
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The material commonly used for air craft gas turbine is
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A jet engine has
OpenVideRime asked 3 years ago • 
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The volume of air delivered by the compressor 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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Efficiency of gas turbine is increased by
OpenVideRime asked 3 years ago • 
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The inlet pressure is always ________ the discharge pressure.
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Gas turbine blades are given a rake
OpenVideRime asked 3 years ago • 
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