A flight path at right angles to the landing runway off its approach end. The base leg normally extends from the downwind leg to the intersection of the extended runway
In fluid dynamics, an increase in the speed of a fluid occurs simultaneously with a decrease in static pressure or a decrease in the fluid’s potential energy. This principle is
Compressed air taken from the compressor stage of a gas turbine engine for aircraft services such as pressurization, anti-icing, and hydraulic reservoir pressurization.
In a turbofan engine, the ratio between the mass flow rate of air drawn through the fan disk but bypassing the engine core to the mass flow rate passing through