Hi all,
I recently created a aircraft model and applied liftdrag plug into its control surfaces. I followed cessna aerodynamic parameters. But, I couldn't get the required flight. I think It would be useful if I fix these parameters according to my model. So, please give the source(or citation of research paper) from where the aerodynamic parameters such as cla,cda, etc are taken
0.4 4.752798721 0.6417112299 0 1.5 -3.85 -0.9233984055 0 .
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