List of top Aeronautical and Aerospace Engineering Questions on Gas Turbines

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