fuselage structure
i'm designing the fuselage for a biz jet as an undergraduate project. i need to know how, generaly, the inner skin is attached to the frames and stringers supporting the outer skin.
also i would like to know how the internal pannels are attached to the inner skin (glue, riveted etc).
this may seem like an obvious question, and it must be, as its not writtern down anywhere!?!. any help most welcome.