(Askeri) HÜCUM AÇISI: Bir tayyarenin kanat veya diğer taşıyıcı satıhlardan birine ait kiriş ile bunun havaya nazaran hareket istikameti arasındaki dar açı
The angle between the chord line of an airfoil and the airflow over it; one of the determiners of the amount of lift produced by an airfoil
The amount of pitch at which an airfoil is flying By adjusting the angle of attack, the efficiency of the wing/blade is effected More precisely, the angle between the chord of an airfoil and the wind
Also designated as AoA It is the angle difference between the wing-chord line measurement and the relative wind
1 hydrodynamically, the designed angle between the planing surface of the sponson and the surface of the water, measured fore and aft
The angle between the relative wind direction and an imaginary line through the center of a flying surface, such as a rocket fin; generally, as the angle of attack increases (raising the forward edge of the surface) so does lift and drag
Angle between the reference axis (x-axis) of an airfoil and the onset flow direction Variable, depending of flow direction and flight condition
in the theory of airplane wings, the angle between the wing profile (roughly, measured along its bottom) and the wing's motion relative to the surrounding air
The number of degrees between the line of thrust and vertical wing plane The greater the angle of attack the greater the lift and the greater the drag
the angle formed by the face of the moving squeegee blade and the plane of the screen, under pressure (Due to the flexibility of the blade, this angle generally differs from the squeegee angle, which is measured without movement or pressure)
direction from which an assault is made; acute angle between the direction of the wind and the chord of an airfoil, AOA
The angle between the direction of the cord of the blades and the relative direction of the wind MORE
The angle of attack is defined as the angle between the plane of the wing (airfoil chord) and the direction of motion (free stream velocity) The angle of attack can be varied to increase or decrease the lift acting on the wing An increase in lift often results in an increase in drag
(AOA) Refers to the angle that a surface contacts the air, usually mentioned when talking about spoilers and wings A higher AOA helps solve oversteer but increases drag and decreases top speed A lower AOA is used to alleviate understeer and increase top speed