turbo_moc.geometry.flow_interfaces module#
Physical multirow interfaces expressed in each row’s conformal chart.
The blade and meridional mapping are left unchanged. Only the inlet/outlet extensions are rebuilt, so their swept caps coincide with a specified axial plane or radial cylinder at every span station, including tapered blades.
- turbo_moc.geometry.flow_interfaces.apply_interfaces(mapping, blade, curves, assembly, settings, eta)[source]#
Reconstruct smooth extensions against the prescribed physical caps.
The adjoining blade-reference endpoint and tangent are retained. Handle proportions follow the existing flow-domain settings; their dimensional lengths use the newly derived extension. Automatic pitchwise placement is deliberately not repeated here.