Radius of curvature normal to the streamlines.

3rd rotor hub section from EEE NASA report.

3rd rotor hub section from EEE NASA report.

Radius of curvature normal to the streamlines.

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

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

Design parameters of the two tested configurations.

Radius of curvature normal to the streamlines.

The 3DBGB section for ARL supersonic compressor.

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

The static pressure rise characteristics of the test facility.

Second derivative over turbine blade surface.

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

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

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

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