{"id":29680,"date":"2018-07-11T23:46:03","date_gmt":"2018-07-11T23:46:03","guid":{"rendered":"\/forum\/forums\/topic\/how-extract-cd-and-cl-and-find-the-angle\/"},"modified":"2018-07-11T23:46:03","modified_gmt":"2018-07-11T23:46:03","slug":"how-extract-cd-and-cl-and-find-the-angle","status":"closed","type":"topic","link":"https:\/\/innovationspace.ansys.com\/forum\/forums\/topic\/how-extract-cd-and-cl-and-find-the-angle\/","title":{"rendered":"How extract Cd and Cl and find the angle?"},"content":{"rendered":"

Hello everyone!<\/p>\n

<\/p>\n

I make a simulation of 2D aerodynamic profile analysis with rotate mesh region to do a attack angle without need use velocity components method. I use the uniform and normal velocity and the airfoil rotate. The simulation is transient. Like in image below.<\/p>\n

<\/p>\n

\"\"<\/p>\n

<\/p>\n

I can see the Cl chart over the flow time or iterations and the same for Cd. But is there any possibility, taking manually, for me to plot Cd or Cl by angle? Why can I do this with each timestep estimating the angle and seeing what the result is at each step, but this is a time consuming manual process. Is there any way?<\/p>\n

<\/p>\n

Thanks for help and opportunity!<\/p>\n

<\/p>\n

Mantovani. <\/p>\n

<\/p>\n

 <\/p>\n","protected":false},"template":"","class_list":["post-29680","topic","type-topic","status-closed","hentry"],"aioseo_notices":[],"aioseo_head":"\n\t\t\n\t\n\t\n\t\n\t\n\t\t\n\t\t\n\t\t\n\t\t\n\t\t\n\t\t\n\t\t\n\t\t\n\t\t\n\t\t\n\t\t\n\t\t\n\t\t\n\t\t\n\t\t