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 Heatsink using Ansys Fluent. In this first video, you will see how to create the geometry and the mesh using DesignModeler, Ansys Meshing and Ansys Fluent.
Free surface is the surface of a fluid that is subject to...
Free surface is the surface of a fluid that is subject to zero parallel shear stress, such as the interface between two homogeneous fluids, for example, liquid water and the air in the Earth's atmosphere. Unlike liquids, gases cannot form a free surface on their...
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 a multiphase simulation through lockExchange tutorial that comes by default with OpenFOAM.
In this video you will learn how to simulate motorBike tutorial using OpenFOAM with simpleFoam solver.
In this tutorial you will learn how to create an animation using OpenFOAM through Paraview (paraFoam Command).
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