Radius of curvature normal to the streamlines.

Radius of curvature normal to the streamlines.

The 3DBGB blade for the EEE 3rd stage rotor.

Rub-grooves measurement depth, corresponding to the six test conditions.

Second derivative B-spline with control points.

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

Constraints for the Spline thickness distribution calculation.

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

Total temperature ratio for Rotor35.

Second derivative over turbine blade surface.

The Second derivative at the Leading edge.

Transverse displacement at the nonlinear boundary as a function of the

Simple Torsion of a cube. The cube above covers the interval [−1, 1] ×