Aerofuselage coefficients

  • 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

  • Thanks for such quick answer, so as I understand all the coefficients are constant for all angles of attack and the lift and drag forces depend on the exposed area and speed only.


    best regards