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April 16, 2017, 05:52 |
foating point exception
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#1 |
New Member
hadi
Join Date: Apr 2017
Posts: 1
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I am working on an ejector system with fluent. this system has two inlets and one pressure outlet and the flow inside the ejector is supersonic. while i apply pressure inlet boundary conditions, fluent gives error as follows:
Divergence detected in AMG solver: ads-0 Primitive Error at Node 1: floating point exception what can i do? it is interesting to note that while i apply mass flow boundary conditions for inlets, there is no problem. |
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