Fluid Flow - Compressible Flow over a Wing-Body Junction

  • Last Post 05 February 2019
svecchi posted this 18 August 2017

The airplane body above is subjected to 600 mile per hour winds at 0 degrees to simulate it traveling mid flight. In an effort to study the flow over the wing-body junction, the velocity vectors and streamlines will be calculated. See the attached file for the tutorial on this problem

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Waddoo posted this 05 February 2019

I'm finding an issue in ANSYS AIM 19.2, where when selecting the Inlet, Outlet, and Opening bodies, AIM says the faces of the enclosure are invalid locations for the region. I'm unsure where I went wrong with the project but any additional help would be greatly appreciated. 

Raef.Kobeissi posted this 12 January 2018

Thanks for sharing that!

Raef Kobeissi

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