Search results
Results From The WOW.Com Content Network
Angle of incidence of an airplane wing on an airplane. On fixed-wing aircraft, the angle of incidence (sometimes referred to as the mounting angle [1] 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).
Washout is a characteristic of aircraft wing design which deliberately reduces the lift distribution across the span of an aircraft’s wing. The wing is designed so that the angle of incidence is greater at the wing roots and decreases across the span, becoming lowest at the wing tip.
Heading angle σ: angle between north and the horizontal component of the velocity vector, which describes which direction the aircraft is moving relative to cardinal directions. Flight path angle γ: is the angle between horizontal and the velocity vector, which describes whether the aircraft is climbing or descending.
Dihedral angle on an aircraft almost ... Longitudinal dihedral is the difference between the angle of incidence of the wing root chord and angle of incidence of the ...
An RF-8 Crusader using its variable-incidence wing during a landing approach. A variable-incidence wing has an adjustable angle of incidence relative to its fuselage.This allows the wing to operate at a high angle of attack for take-off and landing while allowing the fuselage to remain close to horizontal.
Angle of incidence is a measure of deviation of something from "straight on" and may refer to: Angle of incidence (aerodynamics), angle between a wing chord and the longitudinal axis, as distinct from angle of attack, which is relative to the airflow; Angle of incidence (optics), describing the approach of a ray to a surface
The flagship aircraft Venturi, named after the Venturi Effect, is a conceptual canard aircraft that allows the angle of incidence of the channel wing to be varied, enabling the aircraft to achieve hover, transition, and fixed wing flight.
As the angle of attack increases further, the upper surface flow becomes more fully separated and the lift coefficient reduces further. [7] Above this critical angle of attack, the aircraft is said to be in a stall. A fixed-wing aircraft by definition is stalled at or above the critical angle of attack rather than at or below a particular airspeed.