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Radius of curvature normal to the streamlines.

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

Design parameters of the two tested configurations.

HCF ranking results of Hulda Machine Rotor.

Turbine blade hub section in (m , θ) plane. 10 Copyright © 2014 by ASME

The 3DBGB section for ARL supersonic compressor.

Turbine blade hub section in (m , θ) plane. 10 Copyright © 2014 by ASME

Transition onset momentum thickness Reynolds number (Re θ t ) predicted

Second derivative over turbine blade surface.

Radius of curvature normal to the streamlines.

Transition onset momentum thickness Reynolds number (Re θ t ) predicted