{"id":390565,"date":"2024-10-21T09:07:16","date_gmt":"2024-10-21T09:07:16","guid":{"rendered":"https:\/\/innovationspace.ansys.com\/forum\/forums\/topic\/hig-wing-lift-coefficient-value-of-a-3d-wing\/"},"modified":"2024-10-21T09:08:32","modified_gmt":"2024-10-21T09:08:32","slug":"hig-wing-lift-coefficient-value-of-a-3d-wing","status":"publish","type":"topic","link":"https:\/\/innovationspace.ansys.com\/forum\/forums\/topic\/hig-wing-lift-coefficient-value-of-a-3d-wing\/","title":{"rendered":"High wing lift coefficient value of a 3D wing"},"content":{"rendered":"<p>&lt;p&gt;&lt;p&gt;Hi everyone, i am analizing a 3D wing that have a naca profile 63412, 0&deg; AoA, velocity 300 km\/h..Why when i calculate the lift coefficient (solution -&gt; report definition-&gt;lift coefficient-&gt;compute) i get a value of 3300? i mean, shouldn&#8217;t the lift coefficient have a value ranging from 0 to 1.5 more or less?&nbsp; Also the drag coefficient has a high value (205), while the lift force is acceptable (2400 N). Could someone help to understand why of these high value? Thanks&lt;\/p&gt;&lt;\/p&gt;<\/p>\n","protected":false},"template":"","class_list":["post-390565","topic","type-topic","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=\"Hi everyone, i am analizing a 3D wing that have a naca profile 63412, 0\u00b0 AoA, velocity 300 km\/h..Why when i calculate the lift coefficient (solution -&gt; report definition-&gt;lift coefficient-&gt;compute) i get a value of 3300? i mean, shouldn&#039;t the lift coefficient have a value ranging from 0 to 1.5 more or less? 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