Radius of curvature normal to the streamlines.

Comparison of FSM-FRS (left) and five-hole probe (right) static

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

Full section spline thickness distribution.

3DBGB camber line for ARL supersonic cascade.

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

Turbulent kinetic energy around the blade for the MUR235 test case

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

Radius of curvature normal to the streamlines.

COMPARISON BETWEEN NUMERICAL COMPUTED RESUTS (C) AND EXPERIMENTAL

Streamlines against the mesh for two zones in the fourth step of