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Panel - Compressible Flow over a Wing-Body Junction
Panel - Compressible Flow over a Wing-Body Junction

Solution/Results

Press the Results button in the Workflow to extract information from the simulation. In order to find information that can be readily used, first press Evaluate Results. Once the evaluation is complete, AIM will automatically output a vector in the Results section under Objects.

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A pressure contour can be applied to the streamline to show the pressure change as the flow goes over the airplane. Right click the empty model area and select Add > Results > Contour. The Location should automatically be updated to Streamline 1. Change the Variable to Pressure and press Evaluate.


 

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