{"id":362444,"date":"2024-04-16T10:35:38","date_gmt":"2024-04-16T10:35:38","guid":{"rendered":"\/forum\/forums\/reply\/362444\/"},"modified":"2024-04-16T10:35:38","modified_gmt":"2024-04-16T10:35:38","slug":"362444","status":"publish","type":"reply","link":"https:\/\/innovationspace.ansys.com\/forum\/forums\/reply\/362444\/","title":{"rendered":"Reply To: Fluent Supersonic Engine Issues"},"content":{"rendered":"<p>&lt;p&gt;It&#8217;s diverged. So, you need to review the mesh (cell quality and resolution &#8211; ie are you capturing all of the combustion species gradients), boundary conditions (are they sensible) and physics (is the combustion model sensible) and see if the model should be stable and work.&nbsp;&lt;\/p&gt;<\/p>\n","protected":false},"template":"","class_list":["post-362444","reply","type-reply","status-publish","hentry"],"aioseo_notices":[],"aioseo_head":"\n\t\t<!-- All in One SEO 4.9.10 - aioseo.com -->\n\t<meta name=\"description\" content=\"It&#039;s diverged. 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