Drilling of composite without any post drilling affects is very complicated process in aviation industry, because composites are not isotropic as metals.
So we can not use any model that is only compatible with isotropic materials like metals.
There are Cheng, Zhenchao and Matsumura's studies about this subject in literature.
Mr. Şenol Bayraktar, I'd be very pleased if you can provide me any of those literature.
May be, the attached paper, can give you some useful information.
Mr.D.Pandey, I send you attached file about FRPs my manuscript and you can download additional files by sciencedirect.
I don't have a model, only empirical testing to determine the optimum cutter, feeds and speeds, much like Senol Bayraktar did in the paper attached to his (her?) reply. I recommend that you perform empirical testing. It does not require large panels to do this. We investigated both hole drilling and edge trimming for FMCs (I am sorry, I cannot be more specific, nor can I share our data).
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