Hi
I'm looking to calculate the sag of a flight control cable under it's own weight (zero tension). The cable is in steel, 5/32" diameter. Does anybody knows the formula to calculate the sag?
Thanks,
Chopin
I looked in two of my mechancial reference books, they have a lot of words, equations and pictures. I can't seem to be able to relay that info into this mode of comunication.
Try looking for an old guy where you work, and ask to see his mechanical reference books.