The air entry velocity m a rocket as compared to aircraft is
Same
More
Less
Zero
- The pressure and temperature conditions of air at the suction of compressor are
- The efficiency of jet engine is
- Pick up the false statement
- The work ratio of simple gas turbine cycle depends on
- Ratio of indicated H.P. and brake H.P. is known as
- The air entry velocity m a rocket as compared to aircraft is
- In a turbo jet engine, subsequent to heat addition to compressed air, to get the power output, the working…
- In the aircraft propellers
- The area of actual indicator diagram on an air compressor as compared to area of ideal indicator diagram…
- Reheating in gas turbine results in
- Maximum work is done in compressing air when the compression is
- The gas in cooling chamber of a closed cycle gas turbine is cooled at
- The overall isothermal efficiency of compressor is defined as the ratio of
- The air-fuel ratio in gas turbines is of the order of
- 1 m of air at atmospheric condition weighs approximately
- The compressor performance at higher altitude compared to sea level will be
- A rocket engine uses ________ for the combustion of its fuel.
- For perfect intercooling in a two stage compressor
- The absolute pressure of air at the outlet of a compressor is called
- The ratio of the increase in pressure in rotor blades to total increase in pressure in the stage is…
- Out of the following, from where you will prefer to take intake for air compressor
- Mining industry usually employs following motive power
- Clearance volume in actual reciprocating compressors is essential
- Reheating in a gas turbine
- The compressor capacity is defined as the
- The axial flow compressor is preferred in aircraft gas turbines because of
- To avoid moisture troubles, the compressed air main line should
- Mechanical efficiency of gas turbines as compared to I.C engines is
- In air compressors, free air delivery means the
- Which is false statement about advantages of multistage compressor in comparison to single stage compressor?