
Inviscid Bump in a Channel
Inviscid Supersonic Wedge
Inviscid ONERA M6
Laminar Flat Plate
Laminar Cylinder
Turbulent Flat Plate
Transitional Flat Plate
Transitional Flat Plate for T3A and T3A
Turbulent ONERA M6
Unsteady NACA0012
Epistemic Uncertainty Quantification of RANS predictions of NACA 0012 airfoil
Nonideal compressible flow in a supersonic nozzle

Unconstrained shape design of a transonic inviscid airfoil at a cte. AoA
Constrained shape design of a transonic turbulent airfoil at a cte. C_{L}
Constrained shape design of a transonic inviscid wing at a cte. C_{L}
Shape Design With Multiple Objectives and Penalty Functions
Unsteady Shape Optimization NACA0012
Unconstrained shape design of a two way mixing channel
The SU2 Tutorial Collection
Written by  for Version  Revised by  Revision date  Revised version 

@economon  6.0.0  @talbring  20191127  7.0.0 
Getting started with SU2
Rather than writing a long manual on all available (and constantly evolving) configuration options available in SU2, the approach has been taken to teach the various aspects of the SU2 code through a range of tutorials. If you would like to see all of the available config options, we keep a configuration file template in the root directory of the source distribution (see config_template.cfg).
The tutorials are numbered roughly in order of their complexity and how experienced with the code the user may need to be, noting that the more advanced tutorials may assume the user has already worked through the earlier ones. Each tutorial attempts to present new features of SU2 and contains explanations for the key configuration file options. More information on the exact learning goals of a tutorial can be seen at the beginning of each.
You can get all the mesh and config files either by cloning or downloading the tutorial repository or by downloading them separately using the provided links on each tutorial page.
Note: Before beginning with the tutorials, please make sure to check out the information on how to download and install.
Summary of tutorials
Compressible Flow
 Inviscid Bump in a Channel
A simulation of internal, inviscid flow through a 2D geometry.  Inviscid Supersonic Wedge
Get familiar with a basic supersonic flows with analytical solution.  Inviscid ONERAM6
Simulation of external, inviscid flow around a 3D geometry (isolated wing).  Laminar Flat Plate
Simulation of external, laminar flow over a flat plate (classical NavierStokes validation).  Laminar Cylinder
Simulation of external, laminar flow around a 2D cylinder.  Turbulent Flat Plate
Simulation of external, turbulent flow over a flat plate (classical RANS validation).  Transitional Flat Plate(BC transition model)
Simulation of external, transitional flow over a flat plate (transitional latminarturbulent case).  Transitional Flat Plate(LM transition model)
Simulation of external, transitional flow over a flat plate(T3A & T3A) (transitional latminarturbulent case).  Turbulent ONERAM6
Simulation of external, viscous flow around a 3D geometry (isolated wing) using a turbulence model.  Unsteady NACA0012
Simulation of unsteady, external, viscous flow around an airfoil.  Epistemic Uncertainty Quantification of RANS predictions of NACA 0012 airfoil
Perform uncertainty quantification of errors arising due to assumptions inherent in turbulence models.  Nonideal compressible flow in a supersonic nozzle
Simulation of compressible flow in a nozzle using nonideal thermodynamic models.
Incompressible Flow
 Inviscid Hydrofoil
A simulation of internal, inviscid, incompressible flow around a NACA 0012 hydrofoil.  Laminar Flat Plate with Heat Transfer
Simulation of external, laminar, incompressible flow over a flat plate (classical NavierStokes case).  Turbulent Flat Plate
Simulation of external, turbulent incompressible flow over a flat plate (classical RANS case).  Turbulent NACA 0012
Simulation of external, viscous, incompressible flow around the NACA 0012 using a turbulence model.  Laminar Backwardfacing Step
Simulation of internal, laminar, incompressible flow over a backwardfacing step with an inlet velocity profile input from file.  Laminar Buoyancydriven Cavity
Simulation of internal, laminar, incompressible flow in a differentiallyheated cavity under the influence of gravity (classical natural convection case).  Streamwise Periodicity
Simulation of internal, turbulent, incompressible flow in a unit cell of a 2D pinfin heat exchanger.  Species Transport
Simulation of internal, turbulent, incompressible flow through a mixing channel.  Species Transport Composition Dependent Model
Simulation of internal, turbulent, 3D incompressible flow through a Kenics static mixer.  Turbulent Bend
Simulation of turbulent flow in a 90 degree pipe bend using wall functions.
Structural Mechanics
 Linear Elasticity
Simulation of an elasticity problem with small deformations  Linear Dynamics
Simulation of a dynamic structural problem with small deformations  Nonlinear Elasticity
Simulation of a nonlinear structural problem with large deformations  Multiple Materials
Simulation of a nonlinear problem with multiple material definitions
Multiphysics
 Static FluidStructure Interaction
Nonlinear structural mechanics coupled with incompressible NavierStokes flow  Dynamic FluidStructure Interaction with the Python wrapper
Linear Nastranlike model coupled with compressible unsteady RANS equations using the Python wrapper  Static Conjugate Heat Transfer
Simulation of multiple heated cylinders in incompressible fluid flow.  Unsteady Conjugate Heat Transfer
Simulation of an unsteady coupled CHT problem incorporating multiple physical zones.
Shape Design Features
 Unconstrained shape design of an transonic inviscid airfoil at a cte. AoA
Get a basic introduction to the SU2 design capabilities by performing an optimal shape design of a 2D geometry (isolated airfoil) without constraints.  Constrained shape design of a transonic turbulent airfoil at a cte. C_{L}
Perform an optimal shape design of a 2D geometry (isolated airfoil at turbulent regime) with flow and geometrical constraints.  Constrained shape design of a transonic inviscid wing at a cte. C_{L}
Learn the basis of 3D design by performing an optimal shape design of an isolated wing with geometrical constraints.  MultiObjective Shape Design of an Inviscid Supersonic Ramp
Perform an optimal shape design with multiple objectives and a penalty function  Unsteady Shape Optimization
Shape optimization of an 2D airfoil in unsteady flow conditions.  Species Transport
Optimization of internal, turbulent, incompressible flow through a mixing channel.
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