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- Angle_of_attack abstract "In fluid dynamics, angle of attack (AOA, or (Greek letter alpha)) is the angle between a reference line on a body (often the chord line of an airfoil) and the vector representing the relative motion between the body and the fluid through which it is moving. Angle of attack is the angle between the body's reference line and the oncoming flow. This article focuses on the most common application, the angle of attack of a wing or airfoil moving through air.In aerodynamics, angle of attack specifies the angle between the chord line of the wing of a fixed-wing aircraft and the vector representing the relative motion between the aircraft and the atmosphere. Since a wing can have twist, a chord line of the whole wing may not be definable, so an alternate reference line is simply defined. Often, the chord line of the root of the wing is chosen as the reference line. Another choice is to use a horizontal line on the fuselage as the reference line (and also as the longitudinal axis). Some authors do not use an arbitrary chord line, but use the zero lift axis instead — zero angle of attack corresponds to zero coefficient of lift.Some British authors have used the term angle of incidence instead of angle of attack. However, this can lead to confusion with the term riggers' angle of incidence meaning the angle between the chord of an aerofoil and some fixed datum in the aeroplane.".
- Angle_of_attack thumbnail Angle_of_attack.svg?width=300.
- Angle_of_attack wikiPageExternalLink AD-CalibrationOfAirDataSystemsAndFlowDirectionSensors.pdf.
- Angle_of_attack wikiPageID "232102".
- Angle_of_attack wikiPageRevisionID "599189043".
- Angle_of_attack hasPhotoCollection Angle_of_attack.
- Angle_of_attack subject Category:Aerodynamics.
- Angle_of_attack subject Category:Aircraft_wing_design.
- Angle_of_attack subject Category:Kites.
- Angle_of_attack comment "In fluid dynamics, angle of attack (AOA, or (Greek letter alpha)) is the angle between a reference line on a body (often the chord line of an airfoil) and the vector representing the relative motion between the body and the fluid through which it is moving. Angle of attack is the angle between the body's reference line and the oncoming flow.".
- Angle_of_attack label "Angle of attack".
- Angle_of_attack label "Angolo d'attacco".
- Angle_of_attack label "Anstellwinkel".
- Angle_of_attack label "Incidence (aérodynamique)".
- Angle_of_attack label "Invalshoek (aanstroming)".
- Angle_of_attack label "Kąt natarcia".
- Angle_of_attack label "Ángulo de ataque".
- Angle_of_attack label "Ângulo de ataque".
- Angle_of_attack label "Угол атаки".
- Angle_of_attack label "زاوية مواجهة".
- Angle_of_attack label "攻角".
- Angle_of_attack label "迎角".
- Angle_of_attack sameAs Úhel_náběhu.
- Angle_of_attack sameAs Anstellwinkel.
- Angle_of_attack sameAs Ángulo_de_ataque.
- Angle_of_attack sameAs Incidence_(aérodynamique).
- Angle_of_attack sameAs Sudut_serang.
- Angle_of_attack sameAs Angolo_d'attacco.
- Angle_of_attack sameAs 迎角.
- Angle_of_attack sameAs 받음각.
- Angle_of_attack sameAs Invalshoek_(aanstroming).
- Angle_of_attack sameAs Kąt_natarcia.
- Angle_of_attack sameAs Ângulo_de_ataque.
- Angle_of_attack sameAs m.01hrlc.
- Angle_of_attack sameAs Q370906.
- Angle_of_attack sameAs Q370906.
- Angle_of_attack wasDerivedFrom Angle_of_attack?oldid=599189043.
- Angle_of_attack depiction Angle_of_attack.svg.
- Angle_of_attack isPrimaryTopicOf Angle_of_attack.
