Radius of curvature normal to the streamlines.

Transition location (xt/c) vs angle of attack for the S809 airfoil.

Full section spline thickness distribution.

Second derivative over turbine blade surface.

Noise directivity patterns computed by LES and Lighthill's approach

PDF) Smooth Curvature of Airfoils Meanline for a General Turbomachinery Geometry Generator

Turbine MISES Fine Grid. Download Scientific Diagram

Full section spline thickness distribution.

Pressure distribution (Cp) for the S809 airfoil at 1° angle of attack.

3rd rotor hub section from EEE NASA report.

Ideal and realistic expansion process inside gas turbine.