كورس تعليم أنسس فلونت – مثال جناح الطائرة
CFD Analysis of Onera Wing Using Ansys Fluent Course
1 – Introduction \ 1 – Introduction
1 – Introduction \ 2 – A walk through Experimental Work
2 – Geometric Modelling using Creo Parametric \ 3 – Modelling Onera Wing in Creo Parametric
2 – Geometric Modelling using Creo Parametric \ 4 – Creating Airfoil
2 – Geometric Modelling using Creo Parametric \ 5 – Blending the Airfoils
3 – Numerical Simulation using ANSYS Fluent \ 6 – Importing STEP File in Workbench
3 – Numerical Simulation using ANSYS Fluent \ 7 – Create a domain
3 – Numerical Simulation using ANSYS Fluent \ 8 – Create boolean
3 – Numerical Simulation using ANSYS Fluent \ 9 – Add Body of Influence
3 – Numerical Simulation using ANSYS Fluent \ 10 – Dividing the Wing Surface
3 – Numerical Simulation using ANSYS Fluent \ 12 – Advanced Meshing options
4 – Numerical Scheme \ 13 – Physics setup
4 – Numerical Scheme \ 14 – Solution Methods
4 – Numerical Scheme \ 15 – Convergence
5 – Postprocessing \ 16 – CFD Post
5 – Postprocessing \ 17 – Comparison of Contour with Reference Data
5 – Postprocessing \ 18 – Plotting and Exporting Data
5 – Postprocessing \ 19 – Verify Additional Data Quantity
5 – Postprocessing \ 20 – Inverting Axis
5 – Postprocessing \ 21 – Creating Expression and Variable
5 – Postprocessing \ 22 – Comparing Experimental Vs CFD
6 – Data Visualization using Origin and Tecplot 360 \ 23 – Importing in Origin Extracting data from Experimental Charts
6 – Data Visualization using Origin and Tecplot 360 \ 24 – Importing in Tecplot 360
6 – Data Visualization using Origin and Tecplot 360 \ 25 – Iso Surface and Stream lines
6 – Data Visualization using Origin and Tecplot 360 \ 26 – Animation in Tecplot
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