⚡Ansys Fluent Tutorial NACA Airfoil Analysis

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In this Ansys Fluent Tutorial We Will learn how to use NACA 0008 Aerofoil Analysis in Ansys and how to use NACA Database to add a points in Ansys.

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Note : This tutorial is just to show you the method of NACA Aerofoil analysis Results can be vary with different mesh conditions.

NACA AIRFOIL DATABASE WEBSITE LINK :

For More Ansys Tutorials :

NACA 0008 Aerofoil Analysis Ansys Fluent
Ansys Fluent Tutorial NACA Aerofoil Analysis

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Your Video was really helpful

Appreciate your effort

sachinkumar_jadhao
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Thanks for explaining the the part where you join the lose end of the airfoil tail with a line
Been looking at many videos and they skip it don’t know why

codex
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Inlet velocity is set normal to semi-circle boundary, you must set it as Magnitude and Direction vector (for parallel inlet flow).

uladzimir
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Amazing Tutorial 😀
One question though, why did we used a semi-circular inlet? Can we just draw an rectangular surface or was there a specific reason to create a semi-circle

siddharthkarambelkar
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if you changed the angle of attack of the airfoil, would you also change the grid? or would you simply rotate the airfoil and keep the same grid?

MrJoyDevision
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for parameter I only have until table G and I don't have the degree table. how can i add the degree table into the parameter(table of design points)?

amiershah
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different values for lift and drag force at solution and results(one which you set as out put parameter)

akshatchauhan
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this is only the Lift and drag force.How can i get the Cl and Cd to compare with airfoil tool experiment data?

huythan
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sir..How to take the nodal pressure values around airfoil as excel file?

mr.a.aruljohnsonmechanical
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Bro can you provide me screenshot of the final result

MEMERELITE
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contours seems wrong doesn't it? and also the value of lift was so less and it was very close to drag. i am not sure this was an accurate simulation?

shuklaaryan
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Sir why does my results screen don't display anything??

evanderh
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Why did you not use inflation in the mesh

turbochargersutututu
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Hello sir, how to take pictures of pressure contour with varying angle of attack ? Plz help me with this

_rajatpatil
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Bro can we do this in ansys18.0 version?

rishanraj
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(DP 0) The mesh file exporter does not support overlapping geometry in named selections. Please resolve the issue and try again. You can use the option “Show Geometry in Overlapping Named Selections” (when you right click on the Mesh branch of the tree) to help diagnose the problem. getting this error please help

CADTutorialsinUrdu
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Are you performing these Analysis in ansys 2020R1 cracked version that, you've already made a video for the installation of ansys 2020-R1 crack?

hariharan
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Respect Sir, Great Tutorials.
I was working on CFD of Centrifugal Pump and need to draw the characteristic graph.
So how to calculate various parameters like Head, efficiency, Discharge?
Kindly reply.

deeprajkumar