{"id":186329,"date":"2021-07-22T13:07:42","date_gmt":"2021-07-22T13:07:42","guid":{"rendered":"\/forum\/forums\/reply\/186329\/"},"modified":"2021-07-22T13:07:42","modified_gmt":"2021-07-22T13:07:42","slug":"186329","status":"publish","type":"reply","link":"https:\/\/innovationspace.ansys.com\/forum\/forums\/reply\/186329\/","title":{"rendered":"Reply To: Too high cd values"},"content":{"rendered":"

Have a look in the various NACA aerofoil examples (there’s probably on in the Help system in the newer releases). You need to alter the reference values to suit the model. <\/p>\n","protected":false},"template":"","class_list":["post-186329","reply","type-reply","status-publish","hentry"],"aioseo_notices":[],"acf":[],"_links":{"self":[{"href":"https:\/\/innovationspace.ansys.com\/forum\/wp-json\/wp\/v2\/replies\/186329","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\/186329\/revisions"}],"wp:attachment":[{"href":"https:\/\/innovationspace.ansys.com\/forum\/wp-json\/wp\/v2\/media?parent=186329"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}