It supplies hydraulic power electric power and bleed air for the pneumatic system. It also gives thrust.
High to power ratio and performance loss in high altitudes.
By accelerating air pressure.
Reaction engine
80 percent
Decrease in velocity- increase in static pressure.
Manage the torque being given by the turbine.
modern aircraft engine. Is split into a set of separate major modules.
Stator of the 1st stage of HPT.
Mainly used in fan . the Ipc and front stages the hpc.