March 10, 2020
The NACA four-digit wing sections define the profile by:
For example, the NACA 2412 airfoil has a maximum camber of 2% located 40% (0.4 chords) from the leading edge with a maximum thickness of 12% of the chord. Four-digit series airfoils by default have maximum thickness at 30% of the chord (0.3 chords) from the leading edge.
The NACA 0015 airfoil is symmetrical, the 00 indicating that it has no camber. The 15 indicates that the airfoil has a 15% thickness to chord length ratio: it is 15% as thick as it is long.
In this tutorial you will learn to simulate an Airfoil 3D (NACA 4412) using Ansys Fluent. In this tutorial we will use a polyhedral mesh which adapts better to the geometry and allows to obtain convergence in less time compared to the tetrahedral mesh.
In this tutorial, you will learn how to simulate a blower (unsteady) using Mesh Motion with Ansys Fluent. Please download the mesh.
In this tutorial you will learn how to simulate a Blowe using Ansys Fluent through multiple reference frame.
In this tutorial you will learn how to simulate the LES turbulence model using pitzDaily tutorial on OpenFOAM.
In this tutorial, you will learn how to simulate an Airfoil 2D using OpenFOAM. In this case, we will use the folder that comes by default.
In this tutorial you will learn to use Allclean and Allrun scripts on OpenFOAM. These scripts come by default in several OpenFOAM folders.
In the previous tutorial we installed OpenFOAM on Windows, in this video you will simulate the first tutorial called pitzDaily.
In this video you will learn how to install OpenFOAM V8 (from openfoam.org) 2020 using VirtualBox on Windows.
In this tutorial you will learn how to simulate a Flow through Porous Media using Ansys CFX.
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