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Panel

Author: John Singleton and Rajesh Bhaskaran

Problem Specification
1. Pre-Analysis & Start-Up
2. Geometry
3. Mesh
4. Setup (Physics)
5. Solution
6. Results
7. Verification and Validation
Exercises

6. Results

Velocity Vectors

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https://confluence.cornell.edu/download/attachments/144972154/VelVect2_Full.png

Stream Lines

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Steady Flow Past a Cylinder - Panel
Steady Flow Past a Cylinder - Panel

Numerical Results


Start the post-processor (CFD-Post): In project window, right-click Results and select Edit. 

Pressure Contours 

HTML
<iframe width="560" height="315" src="https://www.youtube.com/embed/KU-zrgbSWO0" frameborder="0" allowfullscreen></iframe>

Note: When you open CFD-Post, it opens with a plain wireframe image of the model. In the above video, the video starts off with the 'Velocity Vectors' in the background which is not the case when you start CFD-Post.


Velocity Magnitude Contours 

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<iframe width="560" height="315" src="https://www.youtube.com/embed/VXyIicrrAdM" frameborder="0" allowfullscreen></iframe>

Streamlines

HTML
<iframe width="560" height="315" src="https://www.youtube.com/embed/XNaCs2hHK0M" frameborder="0" allowfullscreen></iframe>

Pressure vs. theta

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<iframe width="560" height="315" src="https://www.youtube.com/embed/B-6fAco0eVE" frameborder="0" allowfullscreen></iframe>

 

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https://confluence.cornell.edu/download/attachments/144972154/StreamLines2_Full.png

Vorticity

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https://confluence.cornell.edu/download/attachments/144972154/Vort_Full.png

Drag Coefficient

Reports > Result Reports > Forces > Setup
Then, click Print. The command pane will now display the following results: the pressure force, the viscous force, the total force, the pressure force coefficient, the viscous force coefficient and the drag force coefficient. As one can see from the following image link, FLUENT yields 2.04 for the value of the drag coefficient. newwindow Drag Coefficient Drag Coefficienthttps://confluence.cornell.edu/download/attachments/144972154/DragCoeff_Full.png



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