aircraft loads
aircraft loads
(OP)
Hi :
I am trying to check the strength of fail safe chord of a aircraft frame. I know the axial load on the skin creates moment on the frame. But I want to know what are the loads and moment acting on the inner and failsafe chord.
thanks
I am trying to check the strength of fail safe chord of a aircraft frame. I know the axial load on the skin creates moment on the frame. But I want to know what are the loads and moment acting on the inner and failsafe chord.
thanks





RE: aircraft loads
not a helpfull answer, i know, but geez no-one can answer the question sensibly.
Sensibly the fail-safe chord is designed by limit loads for the failed structure cases, but somehow i don't think that'll help you either.
good luck