Radius of curvature normal to the streamlines.

Constraints for the Spline thickness distribution calculation.

Second derivative B-spline with control points.

The 3DBGB section for ARL supersonic compressor.

The static pressure rise characteristics of the test facility.

Second derivative B-spline with control points.

3rd rotor hub section from EEE NASA report.

Schematic of the SPIV measurement configuration.

COMPARISON BETWEEN NUMERICAL COMPUTED RESUTS (C) AND EXPERIMENTAL

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