{"id":356535,"date":"2024-03-12T03:15:43","date_gmt":"2024-03-12T03:15:43","guid":{"rendered":"\/forum\/forums\/topic\/surface-coatings\/"},"modified":"2024-03-12T03:15:43","modified_gmt":"2024-03-12T03:15:43","slug":"surface-coatings","status":"closed","type":"topic","link":"https:\/\/innovationspace.ansys.com\/forum\/forums\/topic\/surface-coatings\/","title":{"rendered":"Surface Coatings"},"content":{"rendered":"<p>I am trying to model a uniaxial tensile test on lattice structure surface coated by the metal layer (within elastic range i.e linear analysis). I created lattice geometry using shell feature available in ANSYS spaceclaim, then&nbsp; surface body was created copying all faces in ANSYS Spaceclaim. Then I used share topology between surface and solid body to ensure a conformal mesh between them.<br \/>Can I use share topology between surface and solid bodies??<br \/>I am trying to determine the combined modulus of the model, for which I have plotted max. equivalent stress and Total equivalent strain in the model using time stepping and calculate slope of the graph to get combined modulus.<\/p>\n<p>However, I am getting maximum stress value at metal coating and Max. total strain value at plastic body both at different locations.<\/p>\n<p>Is there any way I can verify my results with hand calculations?<\/p>\n<p>I would really appreciate it if anyone could provide me with advice on this.<\/p>\n<p>Thank you !!<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" title=\"Boundary conditions\" src=\"\/forum\/wp-content\/uploads\/sites\/2\/2024\/03\/12-03-2024-1710212804-Boundary Conditions.PNG\" alt=\"\" width=\"448\" height=\"255\"><img loading=\"lazy\" decoding=\"async\" title=\"Total eq. stress located at metal coating\" src=\"\/forum\/wp-content\/uploads\/sites\/2\/2024\/03\/12-03-2024-1710213071-Total eq stress.PNG\" alt=\"\" width=\"455\" height=\"389\"><br \/><img loading=\"lazy\" decoding=\"async\" title=\"Max. Total eq strain located at plastic body\" src=\"\/forum\/wp-content\/uploads\/sites\/2\/2024\/03\/12-03-2024-1710213128-Total eq strain in mainbody.PNG\" alt=\"\" width=\"446\" height=\"451\"><img loading=\"lazy\" decoding=\"async\" title=\"stress strain plot\" src=\"\/forum\/wp-content\/uploads\/sites\/2\/2024\/03\/12-03-2024-1710213290-ABS_Copper.jpg\" alt=\"\" width=\"532\" height=\"396\"><\/p>\n","protected":false},"template":"","class_list":["post-356535","topic","type-topic","status-closed","hentry"],"aioseo_notices":[],"acf":[],"custom_fields":[{"0":{"_bbp_subscription":["281012","88","170445"],"_bbp_author_ip":["23.52.43.16"]," _bbp_last_reply_id":["0"]," _bbp_likes_count":["0"],"_btv_view_count":["981"],"_bbp_topic_status":["unanswered"],"_bbp_topic_id":["356535"],"_bbp_forum_id":["27791"],"_bbp_engagement":["170445","281012"],"_bbp_voice_count":["2"],"_bbp_reply_count":["3"],"_bbp_last_reply_id":["358101"],"_bbp_last_active_id":["358101"],"_bbp_last_active_time":["2024-03-20 09:53:05"]},"test":"kaflebimail-gvsu-edu"}],"_links":{"self":[{"href":"https:\/\/innovationspace.ansys.com\/forum\/wp-json\/wp\/v2\/topics\/356535","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\/356535\/revisions"}],"wp:attachment":[{"href":"https:\/\/innovationspace.ansys.com\/forum\/wp-json\/wp\/v2\/media?parent=356535"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}