Hi, I am making my own aircraft for aerofly rc and have some questions about the coefficients in [aerofuselage] string. As I understand coefficient Cdx is constant since it is present only when aircraft is flying perfectly straight in the direction of x axis. But what about other coefficients Cdz, Clz, Cdy, Cly and Cm, do they have any relation to the AOA eg. higher AOA, higher the coefficient or are they also just a constant value in all AOA scenarios?
I would very much appreciate any explanation since I couldn't find any details on aerofly wiki or already discussed on this forum.
Thanks to anyone taking their time to answer