The stiffness and mass matrices of a rotating twisted and tapered beam elem
ent are derived. The angle of twist, breadth and depth are assumed to vary
linearly along the length of beam. The effects of shear deformation and rot
ary inertia are also considered in deriving the elemental matrices. The fir
st four natural frequencies and mode shapes in bending-bending mode are cal
culated for cantilever beams. The effects of twist, offset, speed of rotati
on and variation of depth and breadth taper ratios are studied. (C) 2001 Ac
ademic Press.