Design of Wood Aircraft Structures, ANC-18 BulletinHello
I'm trying to follow this interesting post
I take this opportunity to ask you a question
I take the example of the KR2 and its 3-part spar
I'm assuming that the spar caps thicknesses need to be increased at the connecting fittings compared to a one-piece spar to account for the spar being drilled.
Do you know how we can calculate or estimate the necessary increase in thickness?
thank you very much
Dominique .... sorry "google" translation !