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Tutorials
Tutorials show you how to use Simcenter STAR-CCM+ for various applications in a step-by-step format with recommendations for setup, initialization and steps of the solution process specific to the application. Macro and simulation files are available for download for a large proportion of cases.
Compressible Flow
The tutorials in this set illustrate various Simcenter STAR-CCM+ features for compressible fluid flows as well as harmonic balance.
Subsonic Flow: NACA-Type Intake
This tutorial illustrates how to solve a three-dimensional compressible flow problem using Simcenter STAR-CCM+.
Setting Up a Line Surface for Plotting
For comparison with the experimental data, a part needs to be created on which to plot the duct wall pressure ratio.

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Tutorials
Tutorials show you how to use Simcenter STAR-CCM+ for various applications in a step-by-step format with recommendations for setup, initialization and steps of the solution process specific to the application. Macro and simulation files are available for download for a large proportion of cases.
- Using Tutorial Macros and Files
  Macros, input files, and final simulation files for a range of tutorials are provided as an optional download package on the Support Center website. These macros and final simulation files are provided as an aid to the written tutorials, so that you can check your final results against the downloaded files, or against a simulation that is built and run using the macros.
- Introduction
  Welcome to the Simcenter STAR-CCM+ introductory tutorial. In this tutorial, you explore the important concepts and workflow. Complete this tutorial before attempting any others.
- Foundation Tutorials
  The foundation tutorials showcase the major features of Simcenter STAR-CCM+ in a series of short tutorials.
- Geometry
  The tutorials in this set illustrate various Simcenter STAR-CCM+ features for creating and working with parts and 3D-CAD.
- Mesh
  The tutorials in this set illustrate various STAR-CCM+ features for building CFD meshes.
- Incompressible Flow
  The tutorials in this set illustrate various Simcenter STAR-CCM+ features for incompressible fluid flows as well as porosity and solution recording
- Compressible Flow
  The tutorials in this set illustrate various Simcenter STAR-CCM+ features for compressible fluid flows as well as harmonic balance.
  - Subsonic Flow: NACA-Type Intake
    This tutorial illustrates how to solve a three-dimensional compressible flow problem using Simcenter STAR-CCM+.
    - Importing the Mesh and Naming the Simulation
      Create a new simulation, import the supplied mesh, and name the simulation intake.
    - Visualizing the Mesh
      The Geometry Scene 1 display is present in the Graphics window. Set the display to show the mesh.
    - Manipulating Regions and Boundaries
      Combine the separate mesh blocks into a single contiguous mesh, then rename the mesh entities before continuing with the simulation.
    - Setting Up the Physics Models
      Models define the primary variables of the simulation, including pressure, temperature and velocity, and what mathematical formulation is used to generate the solution.
    - Setting Fluid Properties
      Since the Ideal Gas model has been chosen, the viscosity, specific heat, and thermal conductivity fluid properties must be set.
    - Setting Boundary Conditions
      In this simulation, the freestream Mach number is 0.21, the freestream pressure is 98,258.18 Pa, and the freestream temperature is 300 K. Use the default reference pressure of 101,325 Pa, which means that the freestream gauge pressure is -3066.82 Pa.
    - Setting Initial Conditions
      In compressible fluid problems, it is advisable to initialize the flow to a non-zero initial velocity and a meaningful pressure. Here, you use the freestream velocity and the duct outlet pressure.
    - Adding Field Functions
      Field functions provide a mechanism by which fields (raw data from the simulation stored in cells and/or on boundaries) may be viewed and defined.
    - Setting Stopping Criteria
      Stopping criteria allow you to specify the length of the simulation, in this case the number of iterations to be performed.
    - Running the Simulation
      Run the simuation and examine the Residuals display.
    - Visualizing the Mach Number
      As an introduction to data visualization, this section explains how to examine the Mach number field.
    - Visualizing the Velocity Vectors
      This section describes how to examine velocity vectors.
    - Setting Up a Line Surface for Plotting
      For comparison with the experimental data, a part needs to be created on which to plot the duct wall pressure ratio.
    - Plotting Simulation Data
      In this section, the simulation data is plotted using the user-defined field function for pressure ratio and the line surface created from the S-duct wall.
    - Plotting Reference Data
      Display an external data set consisting of experimental data together with the simulation data.
    - Closing and Restarting
      Close and restart the simulation.
    - Summary
      The Subsonic Flow tutorial illustrated how to solve three-dimensional compressible flow problems.
  - Transonic Flow: RAE2822 Airfoil
    The tutorial simulates two-dimensional, turbulent, compressible, transonic air flow over an idealized airfoil.
  - Transonic Flow: RAE2822 Airfoil Using Overset Mesh
    This tutorial demonstrates how to use an overset mesh to simulate transonic flow over the RAE2822 airfoil.
  - Anisotropic Volume Meshing: Onera M6 Wing
    When meshing aerospace geometries such as wings, propeller blades, or turbine blades, you are required to generate a very fine mesh that adequately captures the curvature of the leading and trailing edges. To help reduce the cell count while maintaining solution accuracy, Simcenter STAR-CCM+ provides an anisotropic meshing option by which you can refine these edges.
  - Adaptive Mesh Refinement: Hypersonic Flow
    Hypersonic flows and flight envelopes present unique challenges in Computational Flow Dynamics. The extreme gradients and shocks can push flow solvers to their limits and resolving the flow features, particularly shock formation, is of paramount importance in obtaining valid converged solutions. In Simcenter STAR-CCM+, you can apply Adaptive Mesh Refinement (AMR) to accurately resolve developing shocks using refinement based on solution gradients.
  - Harmonic Balance: Single Stage Periodic Flow
    The tutorial illustrates the steps necessary to simulate a single axial compressor blade row so that the effect of a periodic wake can be analyzed using the Harmonic Balance method.
  - Gas Turbine Aerodynamics: Post-Processing
    In turbomachinery studies, the analysis of the flow field throughout the blade passage requires advanced post processing methods.
- Heat Transfer and Radiation
  The tutorials in this set illustrate various Simcenter STAR-CCM+ features for heat transfer, radiation, and thermal comfort.
- Multiphase Flow
  The tutorials in this set illustrate various Simcenter STAR-CCM+ features for simulating multiphase fluid flow problems
- Discrete Element Method
  The tutorials in this set illustrate various Simcenter STAR-CCM+ features for simulating Discrete Element Method problems
- Motion
  The tutorials in this set illustrate various STAR-CCM+ features for simulating problems with moving geometries and meshes, dynamic fluid body interaction, and rigid body motion:
- Reacting Flow
  The tutorials in this set illustrate various Simcenter STAR-CCM+ features for simulating reacting flows such as combustion.
- Solid Stress
  The tutorials in this set illustrate various Simcenter STAR-CCM+ features for computing deformation, strain, and stresses in solid regions. They also show how such computations can be coupled to the fluid behavior in an analysis of fluid-structure interaction.
- Aeroacoustics
  The tutorials in this set illustrate various Simcenter STAR-CCM+ features for solving aeroacoustic simulations.
- Electromagnetism
  The following tutorials illustrate features for solving problems that involve electromagnetic fields.
- Electrochemistry
  The following tutorial demonstrates chemical reactions induced by an electrical current.
- Battery
  The tutorials in this set illustrate various Simcenter STAR-CCM+ features for setting up a battery model:
- Automation
  The tutorials in this set illustrate various Simcenter STAR-CCM+ automation and macro features.
- Design Exploration
  The tutorials in this set illustrate various features for running design exploration studies in Design Manager.
- Coupling with CAE Codes
  The tutorials in this set illustrate various Simcenter STAR-CCM+ features for coupling with CAE codes:
- Analysis Methods
  The tutorials in this set illustrate various Simcenter STAR-CCM+ features for analysing and visualizing simulation data.
- Simcenter STAR-CCM+ In-cylinder
  The tutorials in this set illustrate features for simulating internal combustion engines in Simcenter STAR-CCM+ using the dedicated add-on Simcenter STAR-CCM+ In-cylinder.

Setting Up a Line Surface for Plotting

For comparison with the experimental data, a part needs to be created on which to plot the duct wall pressure ratio.

Create the part by intersecting a plane with the surface corresponding to the duct wall, resulting in a line surface.

Right-click the Scenes node and select New > Geometry.
In the intake window, right-click the Derived Parts node and select New > Section > Plane Section.

An interactive in-place dialog appears with default settings to allow definition of the derived part.
Click Input Parts to activate the Select Objects dialog.
Expand the Regions > Fluid nodes and select Port Wall only.

Note The Fluid region must be deselected.
Click OK.
In the Plane Parameters box, enter values for the y-coordinate: 0.001 for the origin and 1 for the normal. Set all other values to zero.
In the Display box, select No Displayer.
Click Create.

In the intake window, a node representing the implicit surface created is added under the Derived Parts node: plane section.
Click Close in the dialog.
It is now possible to plot data on the new implicit surface.
Save the simulation.