AlphaLine
https://bladednextgen.dnv.com/schema/0.4.1/Components/Blade/AerofoilLibrary/Aerofoil/AlphaLine/AlphaLine.json
The relationship between angle of attack, and the lift and drag coefficients.
Angle
: number (rad)Cl
: numberCd
: numberCm
: number
Properties
Angle
: number (rad)
The angle of attack for which the Cl, Cd, and Cm apply.
Cl
: number
The non-dimensionalised coefficient of lift.
Cd
: number
The non-dimensionalised coefficient of drag.
Cm
: number
The non-dimensionalised coefficient of pitching.