Search results
- Dictionaryangle of attack
noun
- 1. the angle between the line of the chord of an aerofoil and the relative airflow: "move forwards on the stick to reduce the angle of attack"
Powered by Oxford Dictionaries
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.
Oct 12, 2023 · The aircraft angle of attack (AOA) is defined as the angle of the oncoming wind relative to the aircraft's reference line. In other words, the angle that the oncoming air makes with the center of the fuselage or a designed average point on the wing is referred to as the aircraft AOA.
Dec 10, 2022 · The angle of attack is the angle at which the oncoming airflow meets the wing. It is measured using the wing’s ‘chord line’, a straight line drawn from its leading edge to the trailing edge. The angle of attack is independent of pitch attitude, and many factors affect it.
Definition. The Angle of Attack is the angle at which relative wind meets an Aerofoil. It is the angle formed by the Chord of the aerofoil and the direction of the relative wind or the vector representing the relative motion between the aircraft and the atmosphere.
The angle of attack (AOA) is a fundamental aerodynamic parameter that describes the angle between the chord line of an airfoil (such as an aircraft wing or control surface) and the oncoming air or relative wind. In simpler terms, it is the angle at which the airfoil meets the oncoming air.
Angle of Attack (AOA) is the angle between the chord line of an airfoil and the relative wind. It is the angle at which the wing is meeting the oncoming air. AOA is a critical parameter in determining the aerodynamic performance of an aircraft.
The definition of the angle of attack is the angle between the wing’s chord line and the relative wind. The chord line is an imaginary line that runs between the leading edge and the trailing edge of a wing. The relative wind is the airflow that moves equal and opposite the airplane’s flight path.
