turbo_moc.apps.app.rotor_inlet module

turbo_moc.apps.app.rotor_inlet module#

Resolve a row’s inlet from selected, current upstream results.

The project retains manual inputs when coupling is enabled. Derived values are an execution snapshot, not edits to those manual inputs. The legacy coupling model transfers the stator exit static state without modelling flow through the interspace; the gap still sets the physical row placement independently.

turbo_moc.apps.app.rotor_inlet.require_supersonic_inlet(config)[source]#

Block unsuitable coupled conditions while leaving the readout visible.

turbo_moc.apps.app.rotor_inlet.resolve_configuration(project, row_id, registry)[source]#

Return the effective numerical inputs and their upstream provenance.