Radius of curvature normal to the streamlines.

Blade angles for a compressor blade. ξ, β * in , β * out and χ in are

PDF) A Smooth Curvature-Defined Meanline Section Option for a General Turbomachinery Geometry Generator

Turbine blade hub section in (m , θ) plane. 10 Copyright © 2014 by ASME

The S-shape section camber line.

u − v) coordinate system [6].

3rd rotor hub section from EEE NASA report.

Full section spline thickness distribution.

Kiran SIDDAPPAJI, PhD, University of Cincinnati, Ohio, UC

PDF) A Smooth Curvature-Defined Meanline Section Option for a General Turbomachinery Geometry Generator

Radius of curvature normal to the streamlines.