List of top Aeronautical and Aerospace Engineering Questions asked in Tamil Nadu Common Entrance Test

The combustion in a gas turbine is a
What is the purpose of a fuel injection system in the combustor?
The critical mass flow rate through a converging-diverging nozzle
If there is no change in static enthalpy and static pressure across a rotor, then the turbo-machine is called
The laminar flame speed in a combustion chamber of a jet engine is
For isentropic flows the value of work-done factor for a turbo machine (\(\Psi\)) will be
Characteristic velocity of a rocket engine is equal to
Specific impulse of a rocket
The concept of erosive burning in solid rocket propellant operation pertains to
Which one of the following is not an example of an adapted nozzle?