


{"id":318266,"date":"2023-11-17T21:09:51","date_gmt":"2023-11-17T21:09:51","guid":{"rendered":"\/forum\/forums\/topic\/axisymmetric-jet-nozzle\/"},"modified":"2023-11-17T21:09:51","modified_gmt":"2023-11-17T21:09:51","slug":"axisymmetric-jet-nozzle","status":"closed","type":"topic","link":"https:\/\/innovationspace.ansys.com\/forum\/forums\/topic\/axisymmetric-jet-nozzle\/","title":{"rendered":"Axisymmetric Jet Nozzle"},"content":{"rendered":"<p>Hello,&nbsp;<\/p>\n<p>I am a master&#8217;s student and I am trying to do a validation case for an Axisymmetric subsonic Jet Nozzle. Since I am a beginner in Ansys, although the initial case is periodic as shown below,<\/p>\n<p><img decoding=\"async\" src=\"\/forum\/wp-content\/uploads\/sites\/2\/2023\/11\/17-11-2023-1700254971-mceclip0.png\"><\/p>\n<p>&nbsp;I did start with the 2D case to get used to meshing and software. Then I solved the 2D case and got good results compared to NASA. Then I exported my mesh to ICEM CFD to rotate it 1 degree and solved it again with fluent (shown below)<\/p>\n<p><img decoding=\"async\" src=\"\/forum\/wp-content\/uploads\/sites\/2\/2023\/11\/17-11-2023-1700255349-mceclip1.png\"><\/p>\n<p>&nbsp;however, this time I couldn&#8217;t perform the mesh check in the beginning, and couldn&#8217;t calculate it every time I tried to calculate it gave an error below<\/p>\n<p>&nbsp;<\/p>\n<p>Hybrid initialization is done.<\/p>\n<p>&nbsp;<\/p>\n<p>Writing Settings file &#8220;C:\\Users\\bbaca\\AppData\\Local\\Temp\\WB_bbaca_19128_2\\wbnew_files\\dp0\\FFF\\Fluent\\lmesh.set&#8221;&#8230;<\/p>\n<p>writing rp variables &#8230; Done.<\/p>\n<p>writing domain variables &#8230; Done.<\/p>\n<p>writing fluid (type fluid) (mixture) &#8230; Done.<\/p>\n<p>writing periodic_low-face_high-face (type periodic) (mixture) &#8230; Done.<\/p>\n<p>writing high-face (type periodic) (mixture) &#8230; Done.<\/p>\n<p>writing int_fluid (type interior) (mixture) &#8230; Done.<\/p>\n<p>writing pressure-far-field (type pressure-far-field) (mixture) &#8230; Done.<\/p>\n<p>writing jet-wall (type wall) (mixture) &#8230; Done.<\/p>\n<p>writing jet-inlet (type pressure-inlet) (mixture) &#8230; Done.<\/p>\n<p>writing outlet (type pressure-outlet) (mixture) &#8230; Done.<\/p>\n<p>writing symmetry (type symmetry) (mixture) &#8230; Done.<\/p>\n<p>writing zones map name-id &#8230; Done.<\/p>\n<p>&nbsp;<\/p>\n<p>&nbsp;<\/p>\n<p>iter continuity x-velocity y-velocity z-velocity energy nut time\/iter<\/p>\n<p>&nbsp;<\/p>\n<p>===============Message from the Cortex Process================================<\/p>\n<p>&nbsp;<\/p>\n<p>Compute processes interrupted. Processing can be resumed.<\/p>\n<p>&nbsp;<\/p>\n<p>==============================================================================<\/p>\n<p>&nbsp;<\/p>\n<p>Error at Node 1: Divergence detected in AMG solver<\/p>\n<p>&nbsp;<\/p>\n<p>Divergence detected &#8211; temporarily reducing Courant number to 0.5<\/p>\n<p>and trying again&#8230;<\/p>\n<p>&nbsp;<\/p>\n<p>Divergence detected &#8211; temporarily reducing Courant number to 0.05<\/p>\n<p>and trying again&#8230;<\/p>\n<p>&nbsp;<\/p>\n<p>Divergence detected &#8211; temporarily reducing Courant number to 0.005<\/p>\n<p>and trying again&#8230;<\/p>\n<p>&nbsp;<\/p>\n<p>Divergence detected &#8211; temporarily reducing Courant number to 0.0005<\/p>\n<p>and trying again&#8230;<\/p>\n<p>Stabilizing Coupled to enhance linear solver robustness.<\/p>\n<p>Stabilizing Coupled using GMRES to enhance linear solver robustness.<\/p>\n<p>&nbsp;<\/p>\n<p>Divergence detected &#8211; temporarily reducing Courant number to 5e-05<\/p>\n<p>and trying again&#8230;<\/p>\n<p>Stabilizing Coupled to enhance linear solver robustness.<\/p>\n<p>Stabilizing Coupled using GMRES to enhance linear solver robustness.<\/p>\n<p>&nbsp;<\/p>\n<p>Error at Node 0: Divergence detected in AMG solver<\/p>\n<p>Writing &#8220;| gzip -2cf &gt; SolutionMonitor.gz&#8221;&#8230;<\/p>\n<p>Writing temporary file C:\\Users\\bbaca\\AppData\\Local\\Temp\\flntgz-43722 &#8230;<\/p>\n<p>Done.<\/p>\n<p>&nbsp;<\/p>\n<p>&nbsp;<\/p>\n<p>Calculation complete.<\/p>\n<p>&nbsp;<\/p>\n<p>I am not sure is the mesh file is okay that&#8217;s why I am attaching my mesh file as well.<\/p>\n<p>https:\/\/drive.google.com\/drive\/folders\/1MtyQbhZGmYC3-zDd5ZbaXUh3hXFnkjqk?usp=drive_link<\/p>\n","protected":false},"template":"","class_list":["post-318266","topic","type-topic","status-closed","hentry","topic-tag-fluent-cfd-ansys-1","topic-tag-error","topic-tag-fluent-mesh"],"aioseo_notices":[],"acf":[],"custom_fields":[{"0":{"_oembed_141bd2d9cf68165690ec1bca990e0e16":["{{unknown}}"],"_bbp_subscription":["296885","199"],"_bbp_author_ip":["23.52.43.88"]," _bbp_last_reply_id":["0"]," _bbp_likes_count":["0"],"_btv_view_count":["564"],"_bbp_topic_status":["unanswered"],"_bbp_status":["publish"],"_oembed_305170661aa027dedfaddab6f84ca731":["{{unknown}}"],"_bbp_topic_id":["318266"],"_bbp_forum_id":["27792"],"_bbp_engagement":["199","296885"],"_bbp_voice_count":["2"],"_bbp_reply_count":["2"],"_bbp_last_reply_id":["319849"],"_bbp_last_active_id":["319849"],"_bbp_last_active_time":["2023-11-28 17:45:37"]},"test":"cem-bizstudent-uliege-be"}],"_links":{"self":[{"href":"https:\/\/innovationspace.ansys.com\/forum\/wp-json\/wp\/v2\/topics\/318266","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/innovationspace.ansys.com\/forum\/wp-json\/wp\/v2\/topics"}],"about":[{"href":"https:\/\/innovationspace.ansys.com\/forum\/wp-json\/wp\/v2\/types\/topic"}],"version-history":[{"count":0,"href":"https:\/\/innovationspace.ansys.com\/forum\/wp-json\/wp\/v2\/topics\/318266\/revisions"}],"wp:attachment":[{"href":"https:\/\/innovationspace.ansys.com\/forum\/wp-json\/wp\/v2\/media?parent=318266"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}