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#1 |
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New Member
Join Date: Dec 2020
Posts: 14
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Hi, I'm fairly new to Ansys CFX but currently attempting to simulate the supersonic Mach 1.2 flow over a subsonic aerofoil.
For some reason, I am able to get successful runs for 6, 9 and 12 degrees but not at 3- whenever I attempt it, I end up getting a "Fatal Overflow" message. I'm using the exact same mesh, domain and input values for all of the runs but for some reason it is only 3 degrees that appears to be failing- why could this be? |
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#2 |
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Super Moderator
Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
Posts: 18,001
Rep Power: 146 ![]() ![]() ![]() ![]() |
This question is a duplicate of your other thread: Problems running Supersonic
Please post responses on that thread.
__________________
Note: I do not answer CFD questions by PM. CFD questions should be posted on the forum. |
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