Radius of curvature normal to the streamlines.
By A Mystery Man Writer
Description
Kiran SIDDAPPAJI, PhD, University of Cincinnati, Ohio, UC
The 3DBGB blade for the EEE 3rd stage rotor.
Turbine passage Mach number contours.
Radius of curvature normal to the streamlines.
r − x − θ) 3D coordinate system [6].
Total temperature ratio for Rotor35.
The Second derivative at the Leading edge.
Transition onset momentum thickness Reynolds number (Re θ t ) predicted
Radius of curvature normal to the streamlines.
Second derivative over turbine blade surface.
FRF associated for the tuned structure for engine order (EO=3) as
Constraints for the Spline thickness distribution calculation.
Kiran SIDDAPPAJI, PhD, University of Cincinnati, Ohio, UC
Turbine passage Mach number contours.
from
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