{"id":313324,"date":"2023-10-25T15:49:35","date_gmt":"2023-10-25T15:49:35","guid":{"rendered":"\/forum\/forums\/reply\/313324\/"},"modified":"2023-10-25T15:49:35","modified_gmt":"2023-10-25T15:49:35","slug":"313324","status":"publish","type":"reply","link":"https:\/\/innovationspace.ansys.com\/forum\/forums\/reply\/313324\/","title":{"rendered":"Reply To: Trouble Importing Pressure Load Data from CFD Wing Simulation to Individual Rib"},"content":{"rendered":"<p>&lt;p&gt;Now i see there is a small increase about 1 Pa of the pressure load between fluent results of the part of the wing (72.5mm) and imported pressure onto rib surface in static analysis but i dont know if it shouldn&#8217;t be greater&lt;\/p&gt;&lt;h1&gt;<img loading=\"lazy\" decoding=\"async\" src=\"\/forum\/wp-content\/uploads\/sites\/2\/2023\/10\/25-10-2023-1698248544-Zrzut ekranu 2023-10-25 172240.png\" alt=\"\" width=\"781\" height=\"346\" \/>&lt;\/h1&gt;&lt;p&gt;<img loading=\"lazy\" decoding=\"async\" src=\"\/forum\/wp-content\/uploads\/sites\/2\/2023\/10\/25-10-2023-1698248674-Zrzut ekranu 2023-10-25 173050.png\" alt=\"\" width=\"788\" height=\"238\" \/>&lt;\/p&gt;<\/p>\n","protected":false},"template":"","class_list":["post-313324","reply","type-reply","status-publish","hentry"],"aioseo_notices":[],"acf":[],"_links":{"self":[{"href":"https:\/\/innovationspace.ansys.com\/forum\/wp-json\/wp\/v2\/replies\/313324","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/innovationspace.ansys.com\/forum\/wp-json\/wp\/v2\/replies"}],"about":[{"href":"https:\/\/innovationspace.ansys.com\/forum\/wp-json\/wp\/v2\/types\/reply"}],"version-history":[{"count":0,"href":"https:\/\/innovationspace.ansys.com\/forum\/wp-json\/wp\/v2\/replies\/313324\/revisions"}],"wp:attachment":[{"href":"https:\/\/innovationspace.ansys.com\/forum\/wp-json\/wp\/v2\/media?parent=313324"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}