This paper presents a method to study the free vibration of a rotating trun
cated circular layered conical shell with simply-supported boundary conditi
ons. Based on the Love first approximation theory and Galerkin procedure, a
nd taking into account the influences of centrifugal and Coriolis accelerat
ions and the effects of initial hoop tension, the frequency characteristics
are obtained for various geometric properties, vibrational modes and diffe
rent rotating speeds. The effect of cone angle on frequency characteristics
is also discussed in details. Comparisons with published results available
in the literature indicate that the present method is reliable and applica
ble. (C) 2000 Elsevier Science Ltd. All rights reserved.