The aim of this work was to determine assembly stresses in taper-locking as
semblies, to seek simple methods of calculating the important stresses and
to test their validity. Four models were analysed: a coupling only, two mod
els with hollow shafts and one on a solid shaft, surrounded by a hub. Hoop-
radial maximum shear stresses were compared with thick-cylinder calculation
s. There was good agreement except for the frictional effects due to circum
ferential sliding of slit rings between continuous (unslit) rings.