turbo_moc.geometry.geometry_3d module#
One reference placement with an annular mapping or linear extrusion.
Reference passage placement: optimize at eta=0.5 once, carry that reference-plane translation across span, and preserve the chosen pitch. Axial and radial convenience dimensions share the same annular mapping.
- class turbo_moc.geometry.geometry_3d.Design(meridional_channel: ~turbo_moc.geometry.meridional_channel.MeridionalChannel | ~turbo_moc.geometry.linear_cascade.LinearCascadeMapping, blade: dict, curves: dict, assembly: dict = <factory>, flow_domain: dict = <factory>)[source]#
Bases:
objectCanonical reference blade and passage, before any mesh exists.
Methods
section(eta)Scale shape/chord while retaining pitch and the reference translation.
- assembly: dict#
- blade: dict#
- curves: dict#
- flow_domain: dict#
- meridional_channel: MeridionalChannel | LinearCascadeMapping#
- turbo_moc.geometry.geometry_3d.build_design(nozzle, config, *, definition=None, template=None)[source]#
Fit once and perform the sole auto-centering search at the reference span.
- turbo_moc.geometry.geometry_3d.encode(value)[source]#
JSON-safe scientific artifact format, without loading arbitrary pickle.
- turbo_moc.geometry.geometry_3d.mapping_from_data(definition)[source]#
Reconstruct an explicit linear or annular mapping from its artifact.
- turbo_moc.geometry.geometry_3d.meridional_grid(design, numerics, section=None, *, samples=45)[source]#
Projection of actual periodic-boundary stations swept across actual eta.
Before a reference mesh exists, use sampled station locations. Afterwards every displayed streamwise station comes from its periodic_left mesh nodes. This is a meridional grid projection, not a second independent CFD mesh.