Profile drag is composed of form drag and skin friction. Form drag results from the turbulent wake caused by the separation of airflow from the surface of a structure
The blade pitch may be fixed, manually variable to a few set positions, or of the automatically variable "constant-speed" type.
The horizontal distance that an aircraft uses to turn is referred to as the radius of turn. It varies as a function of bank angle and the square of the airspeed
The gross thrust coefficient (Cfg) is a measure of the nozzle efficiency and accounts for nozzle losses due to friction, angularity, expansion, leakage and cooling air throttling
The Mach number of a normal shock wave is always greater than unity in the upstream and less than unity in the downstream, the static pressure always increases across the…