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[WIP] Update turbo interfaces #2209
Merged
joshkellyjak
merged 374 commits into
su2code:feature_resolve_merge_turbo_interfaces
from
joshkellyjak:feature_turbo_interfaces
Sep 4, 2024
Merged
[WIP] Update turbo interfaces #2209
joshkellyjak
merged 374 commits into
su2code:feature_resolve_merge_turbo_interfaces
from
joshkellyjak:feature_turbo_interfaces
Sep 4, 2024
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joshkellyjak
changed the title
[Draft] Update turbo interfaces
[WIP] Update turbo interfaces
Feb 13, 2024
pcarruscag
reviewed
Feb 13, 2024
Workaround for ASLR/tsan incompatibility
Added gprof profiling option
…gle value is provided
…_solid-solid_cht
Solid to solid conjugate heat transfer with contact resistance
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/*--- Compute and update residual. Note that the viscous shear stress tensor is computed in the | ||
following routine based upon the velocity-component gradients. ---*/ | ||
auto residual = visc_numerics->ComputeResidual(config); |
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line 1224
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Loading @@ -161,8 +175,10 @@ | |||
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/*--- Roe-averaged speed of sound ---*/ | |||
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//RoeSoundSpeed2 = Gamma_Minus_One * ( RoeEnthalpy - 0.5 * sq_velRoe ); |
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Commented-out code Note
This comment appears to contain commented-out code.
joshkellyjak
changed the base branch from
develop
to
feature_turbo_interfaces
September 4, 2024 14:23
joshkellyjak
merged commit Sep 4, 2024
d106401
into
su2code:feature_resolve_merge_turbo_interfaces
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Proposed Changes
Update to the interface initialisation to enable both mixing plane and sliding interfaces within the same turbomachinery simulation. Addition of mass flow outlet to Giles BC.
Related Work
This issue solves a problem reported by a number of users, when simulating radial turbomachinery cases a second-order accurate solution cannot be achieved in some cases when using mixing plane interfaces. This is due to circumfrential averaging in regions where the flow exhibits large circumfrential nonuniformity and/or interspace gaps between adjacent blade-rows/zones small. This issue has been reported by @LorenzoFabris, in a presentation at the SU2 Conference 2022 "Performance Analysis and Shape Optimization of a Radial Compressor with the Open-Source Software SU2" and by myself.
Mass flow outlet included in the PR as requested by users.
TBC:
-Update APU Turbocharger test case and regression test to include this feature, add diffuser and converge 2nd order.
PR Checklist
Put an X by all that apply. You can fill this out after submitting the PR. If you have any questions, don't hesitate to ask! We want to help. These are a guide for you to know what the reviewers will be looking for in your contribution.
pre-commit run --all
to format old commits.