Table of Contents

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: number
  • Cd: number
  • Cm: 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.