[joshkellyjak]

Proposed Changes

Added support for multiphysics calculations for multizone turbomachinery cases.

Blade rows are the first zones, one per MARKER_TURBOMACHINERY pair (CConfig::GetnTurboZones). Zones that are not compressible flow drop the turbomachinery, Giles and mixing-plane markers inherited from the master config, so e.g. blade solids coupled via MARKER_CHT_INTERFACE are plain heat zones.

• Turbo preprocessing, stage performance, turbo monitor and turbo history output loop over the turbo zones instead of all zones; the stage outlet is the last turbo zone.
• TURBOMACHINERY_KIND / TURBO_PERF_KIND are checked against the number of turbo zones.
• Only interfaces between two turbo zones skip the generic interpolator, so CHT interfaces with a turbo fluid zone get one.

Pure turbomachinery cases are unchanged (outputs byte-identical to the base commit).

Test case for direct and adjoint coming soon.

Related Work

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