Transition onset momentum thickness Reynolds number (Re θ t ) predicted
3rd rotor hub section from EEE NASA report.
The S-shape section camber line.
Full section spline thickness distribution.
Constraints for the Spline thickness distribution calculation.
Turbine MISES Fine Grid. Download Scientific Diagram
r − x − θ) 3D coordinate system [6].
Turbulent kinetic energy around the blade for the MUR235 test case
Second derivative B-spline with control points.
Radius of curvature normal to the streamlines.
Total temperature ratio for Rotor35.
3rd rotor hub section from EEE NASA report.
Second derivative B-spline with control points.
Rub-grooves measurement depth, corresponding to the six test conditions.
Comparison of FSM-FRS (left) and five-hole probe (right) static
