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Supersonic Flow Over a Wedge - Panel
Supersonic Flow Over a Wedge - Panel

Geometry

 

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Info

This page goes through the geometry steps for the Supersonic Flow Over a Wedge in the SpaceClaim geometry engine included with ANSYS Workbench. For instructions on creating the geometry using DesignModeler, see this page.

Some tips:

  • As you follow along in Ansys, you can switch between the video and Ansys easily using Alt+Tab if you are on a MS Windows computer.
  • In newer Ansys versions, there is a new Sketch tab in SpaceClaim with slight changes in the sketching procedure which you should be able to able to figure out with a bit of poking around.  
  • In SpaceClaim, you can zoom in/out using the mouse wheel, rotate using MMB (middle mouse button) and translate using Ctrl+MMB. 


HTML
<iframe width="560" height="315" src="https://www.youtube.com/embed/V48xj75kzdQ" frameborder="0" allow="accelerometer; autoplay; encrypted-media; gyroscope; picture-in-picture" allowfullscreen></iframe>

 

In later steps, the geometry will be split into two domains. To do this in SpaceClaim, simply go to the Design tab and choose Split under the Intersect section of the menu bar. Select the domain, and then select the point at the leftmost point of the wedge (the angled side). 

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Go to Step 3: Mesh

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