BladeSectionQuarterChordCoordinateSystem
https://bladednextgen.dnv.com/schema/0.4.1/Components/Blade/BladeSectionDefinition/BladeSectionAxesAndCoordinateSystems/BladeSectionQuarterChordCoordinateSystem/BladeSectionQuarterChordCoordinateSystem.json
This axes system positions the aerofoil relative to the reference axes. The origin is at the quarter-chord position, a quarter of the way from the leading edge to the trailing edge along the chordline. The X-axis of the system is parallel to the chordline, and the Y-axis perpendicular to it. If omitted, the reference axes will be used as the quarter-chord axes.
OffsetInReferenceX
: number (m)OffsetInReferenceY
: number (m)RotationAboutReferenceZ
: number (rad)
Properties
OffsetInReferenceX
: number (m), optional
The offset of the axis system origin from the reference axes in x.
default = 0.0
OffsetInReferenceY
: number (m), optional
The offset of the axis system origin from the reference axes in y.
default = 0.0
RotationAboutReferenceZ
: number (rad), optional
The rotation of the axis system's x and y axes around the reference z axis (the section plane normal).
default = 0.0