12/24/2023 0 Comments Supersonic airfoilShape optimization of an 2D airfoil in unsteady flow conditions. Perform an optimal shape design with multiple objectives and a penalty function Multi-Objective Shape Design of an Inviscid Supersonic Ramp.Learn the basis of 3D design by performing an optimal shape design of an isolated wing with geometrical constraints. Constrained shape design of a transonic inviscid wing at a cte.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 turbulent airfoil at a cte.Get a basic introduction to the SU2 design capabilities by performing an optimal shape design of a 2D geometry (isolated airfoil) without constraints. Unconstrained shape design of an transonic inviscid airfoil at a cte.Simulation of an unsteady coupled CHT problem incorporating multiple physical zones. Simulation of multiple heated cylinders in incompressible fluid flow. Linear Nastran-like model coupled with compressible unsteady RANS equations using the Python wrapper Dynamic Fluid-Structure Interaction with the Python wrapper.Non-linear structural mechanics coupled with incompressible Navier-Stokes flow Simulation of a non-linear problem with multiple material definitions Simulation of a non-linear structural problem with large deformations Simulation of a dynamic structural problem with small deformations Simulation of an elasticity problem with small deformations Simulation of internal, turbulent, incompressible flow through a mixing channel. Simulation of internal, turbulent, incompressible flow in a unit cell of a 2D pin-fin heat exchanger. Simulation of internal, laminar, incompressible flow in a differentially-heated cavity under the influence of gravity (classical natural convection case). Simulation of internal, laminar, incompressible flow over a backward-facing step with an inlet velocity profile input from file. Simulation of external, viscous, incompressible flow around the NACA 0012 using a turbulence model. Simulation of external, turbulent incompressible flow over a flat plate (classical RANS case). Simulation of external, laminar, incompressible flow over a flat plate (classical Navier-Stokes case). Simulation of compressible flow in a nozzle using non-ideal thermodynamic models.Ī simulation of internal, inviscid, incompressible flow around a NACA 0012 hydrofoil. Non-ideal compressible flow in a supersonic nozzle.Perform uncertainty quantification of errors arising due to assumptions inherent in turbulence models. Epistemic Uncertainty Quantification of RANS predictions of NACA 0012 airfoil.Simulation of unsteady, external, viscous flow around an airfoil. Simulation of external, viscous flow around a 3D geometry (isolated wing) using a turbulence model. Simulation of external, transitional flow over a flat plate (transitional latminar-turbulent case). Simulation of external, turbulent flow over a flat plate (classical RANS validation). Simulation of external, laminar flow around a 2D cylinder. Simulation of external, laminar flow over a flat plate (classical Navier-Stokes validation). Simulation of external, inviscid flow around a 3D geometry (isolated wing). Get familiar with a basic supersonic flows with analytical solution. Summary of tutorialsĪ simulation of internal, inviscid flow through a 2D geometry. Note: Before beginning with the tutorials, please make sure to check out the information on how to download and install. 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. More information on the exact learning goals of a tutorial can be seen at the beginning of each. Each tutorial attempts to present new features of SU2 and contains explanations for the key configuration file options. 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. 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). 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.
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