##### Angle of Incidence
On [[fixed-wing]] aircraft, the angle of incidence (sometimes referred to as the mounting angle or setting angle) is the angle between the [[chord line]] of the [[wing]] where the wing is mounted to the [[fuselage]], and a reference axis along the fuselage (often the direction of minimum [[drag]], or where applicable, the [[longitudinal axis]]). The angle of incidence is fixed in the design of the aircraft, and with rare exceptions, cannot be varied in flight.
The term can also be applied to horizontal surfaces in general (such as [[canards]] or [[horizontal stabilizers]]) for the angle they make relative to the longitudinal axis of the fuselage.
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>References: [[WP Angle of Incidence|🌍]]
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