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Change links in unst cht, as files moved. Plus little fixes.
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_tutorials/index.md

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@@ -63,7 +63,7 @@ Simulation of external, viscous, incompressible flow around the NACA 0012 using
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Simulation of internal, laminar, incompressible flow over a backward-facing step with an inlet velocity profile input from file.
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* [Laminar Buoyancy-driven Cavity](/tutorials/Inc_Laminar_Cavity/)
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Simulation of internal, laminar, incompressible flow in a differentially-heated cavity under the influence of gravity (classical natural convection case).
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* [Streamwise Periodicity](/tutorials/Inc_Streamwise_Periodic/)
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* [Streamwise Periodicity](/tutorials/Inc_Streamwise_Periodic/)
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Simulation of internal, turbulent, incompressible flow in a unit cell of a 2D pin-fin heat exchanger.
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#### Structural Mechanics
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* [Static Fluid-Structure Interaction](/tutorials/Static_FSI/)
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Non-linear structural mechanics coupled with incompressible Navier-Stokes flow
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* [Dynamic Fluid-Structure Interaction with the Python wrapper](/tutorials/Dynamic_FSI_Python/)
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* [Dynamic Fluid-Structure Interaction with the Python wrapper](/tutorials/Dynamic_FSI_Python/)
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Linear Nastran-like model coupled with compressible unsteady RANS equations using the Python wrapper
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* [Static Conjugate Heat Transfer](/tutorials/Static_CHT/)
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* [Static Conjugate Heat Transfer](/tutorials/Static_CHT/)
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Simulation of multiple heated cylinders in incompressible fluid flow.
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* [Unsteady Conjugate Heat Transfer](/tutorials/Inc_Heated_Cylinders_Unsteady/)
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* [Unsteady Conjugate Heat Transfer](/tutorials/Inc_Heated_Cylinders_Unsteady/)
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Simulation of an unsteady coupled CHT problem incorporating multiple physical zones.
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#### Shape Design Features
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* [Unconstrained shape design of an transonic inviscid airfoil at a cte. AoA](/tutorials/Inviscid_2D_Unconstrained_NACA0012/)
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* [Unconstrained shape design of an transonic inviscid airfoil at a cte. AoA](/tutorials/Inviscid_2D_Unconstrained_NACA0012/)
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Get a basic introduction to the SU2 design capabilities by performing an optimal shape design of a 2D geometry (isolated airfoil) without constraints.
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* [Constrained shape design of a transonic turbulent airfoil at a cte. C<sub>L</sub>](/tutorials/Turbulent_2D_Constrained_RAE2822/)
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Perform an optimal shape design of a 2D geometry (isolated airfoil at turbulent regime) with flow and geometrical constraints.

_tutorials/multiphysics/steady_cht/Static_CHT.md

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---
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title: Static Conjugate Heat Transfer (CHT)
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permalink: /tutorials/Static_CHT
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permalink: /tutorials/Static_CHT/
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written_by: oleburghardt
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for_version: 7.0.0
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revised_by: oleburghardt

_tutorials/multiphysics/unsteady_cht/Inc_Heated_Cylinders_Unsteady.md

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---
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title: Unsteady Conjugate Heat Transfer
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permalink: /tutorials/Inc_Heated_Cylinders_Unsteady/
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written_by: oleburghardt
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for_version: 7.1.0
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revised_by: TobiKattmann
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revision_date: 2021-03-04
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revised_version: 7.1.1
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solver: INC_NAVIER_STOKES, HEAT_EQUATION
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requires: SU2_CFD
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complexity: advanced
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follows: Static_CHT
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userguide: Multizone
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---
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<br>
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## Resources
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The resources for this tutorial can be found in the [Inc_Heated_Cylinders_Unsteady](https://github.com/su2code/su2code.github.io/blob/unsteady_cht_tutorial/Inc_Heated_Cylinders_Unsteady) directory in the [tutorial repository](https://github.com/su2code/su2code.github.io/blob/unsteady_cht_tutorial/). You will need the configuration files for all physical zones ([flow_cylinder.cfg](../../Inc_Heated_Cylinders_Unsteady/flow_cylinder.cfg), [solid_cylinder1.cfg](../../Inc_Heated_Cylinders_Unsteady/solid_cylinder1.cfg), [solid_cylinder2.cfg](../../Inc_Heated_Cylinders_Unsteady/solid_cylinder2.cfg), [solid_cylinder3.cfg](../../Inc_Heated_Cylinders_Unsteady/solid_cylinder3.cfg)), the cofiguration file to invoke a multiphysics simulation run ([cht_2d_3cylinders.cfg](../../Inc_Heated_Cylinders_Unsteady/cht_2d_3cylinders.cfg)) and the mesh file ([mesh_cht_3cyl.su2](../../Inc_Heated_Cylinders_Unsteady/mesh_cht_3cyl.su2)).
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The resources for this tutorial can be found in the [Inc_Heated_Cylinders_Unsteady](https://github.com/su2code/Tutorials/tree/master/multiphysics/unsteady_cht) directory in the [tutorial repository](https://github.com/su2code/Tutorials). You will need the configuration files for all physical zones ([flow_cylinder.cfg](https://github.com/su2code/Tutorials/tree/master/multiphysics/unsteady_cht/flow_cylinder.cfg), [solid_cylinder1.cfg](https://github.com/su2code/Tutorials/tree/master/multiphysics/unsteady_cht/solid_cylinder1.cfg), [solid_cylinder2.cfg](https://github.com/su2code/Tutorials/tree/master/multiphysics/unsteady_cht/solid_cylinder2.cfg), [solid_cylinder3.cfg](https://github.com/su2code/Tutorials/tree/master/multiphysics/unsteady_cht/solid_cylinder3.cfg)), the cofiguration file to invoke a multiphysics simulation run ([cht_2d_3cylinders.cfg](https://github.com/su2code/Tutorials/tree/master/multiphysics/unsteady_cht/cht_2d_3cylinders.cfg)) and the mesh file ([mesh_cht_3cyl.su2](https://github.com/su2code/Tutorials/tree/master/multiphysics/unsteady_cht/mesh_cht_3cyl.su2)).
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## Tutorial
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```
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INC_DENSITY_INIT= 0.0210322
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```
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in [flow_cylinder.cfg](../../Inc_Heated_Cylinders_Unsteady/flow_cylinder.cfg) and
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in [flow_cylinder.cfg](https://github.com/su2code/Tutorials/tree/master/multiphysics/unsteady_cht/flow_cylinder.cfg) and
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```
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SOLID_DENSITY= 0.0210322
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```
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in [solid_cylinder1.cfg](../../Inc_Heated_Cylinders_Unsteady/solid_cylinder1.cfg), [solid_cylinder2.cfg](../../Inc_Heated_Cylinders_Unsteady/solid_cylinder2.cfg) and [solid_cylinder3.cfg](../../Inc_Heated_Cylinders_Unsteady/solid_cylinder3.cfg)
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in [solid_cylinder1.cfg](https://github.com/su2code/Tutorials/tree/master/multiphysics/unsteady_cht/solid_cylinder1.cfg), [solid_cylinder2.cfg](https://github.com/su2code/Tutorials/tree/master/multiphysics/unsteady_cht/solid_cylinder2.cfg) and [solid_cylinder3.cfg](https://github.com/su2code/Tutorials/tree/master/multiphysics/unsteady_cht/solid_cylinder3.cfg)
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For simplicity we leave all other parameters unchanged.
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### Mesh Description
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The [mesh](../../Inc_Heated_Cylinders_Unsteady/mesh_cht_3cyl.su2) is the same as in the [heated cylinders with conjugate heat transfer tutorial](/tutorials/Inc_Heated_Cylinders/).
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The [mesh](https://github.com/su2code/Tutorials/tree/master/multiphysics/unsteady_cht/mesh_cht_3cyl.su2) is the same as in the [heated cylinders with conjugate heat transfer tutorial](/tutorials/Inc_Heated_Cylinders/).
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### Configuration File Options
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An unsteady simulation is set up by enabling the time domain and choosing a time marching algorithm in the [master config file](../../Inc_Heated_Cylinders_Unsteady/cht_2d_3cylinders.cfg):
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An unsteady simulation is set up by enabling the time domain and choosing a time marching algorithm in the [master config file](https://github.com/su2code/Tutorials/tree/master/multiphysics/unsteady_cht/cht_2d_3cylinders.cfg):
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```
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TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
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```
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The time marching parameters have to match the flow physics that should be resolved. For a given inlet velocity of 3.40297 m/s at Re = 4000, the Strouhal number estimation for the most upstream cylinder is Sr = 0.21. This gives a frequency of f = Sr*v = 0.71Hz for the vortex shedding so that a time step of 0.05s is chosen in the [master config file](../../Inc_Heated_Cylinders_Unsteady/cht_2d_3cylinders.cfg):
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The time marching parameters have to match the flow physics that should be resolved. For a given inlet velocity of 3.40297 m/s at Re = 4000, the Strouhal number estimation for the most upstream cylinder is Sr = 0.21. This gives a frequency of f = Sr*v = 0.71Hz for the vortex shedding so that a time step of 0.05s is chosen in the [master config file](https://github.com/su2code/Tutorials/tree/master/multiphysics/unsteady_cht/cht_2d_3cylinders.cfg):
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```
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TIME_STEP= 0.05
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```
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In order to sufficiently resolve the coupling in each time step, we set the number of outer iterations to 200 in the [master config file](../../Inc_Heated_Cylinders_Unsteady/cht_2d_3cylinders.cfg):
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In order to sufficiently resolve the coupling in each time step, we set the number of outer iterations to 200 in the [master config file](https://github.com/su2code/Tutorials/tree/master/multiphysics/unsteady_cht/cht_2d_3cylinders.cfg):
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```
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OUTER_ITER = 200

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