A relatively simple mathematical model involving an idealized rotating stri
ng constrained at one point is used to develop an understanding of the basi
c physical mechanisms that govern the development of unstable lateral vibra
tion response. Equations defining the relationship between the interactive
inertial, damping, elastic and applied forces are presented. Analysis of th
ese equations leads to a clear understanding of the physical mechanisms inv
olved in the development of divergence and flutter instability mechanisms.
New developments involve the identification of the energy flux into the rot
ating system and an explanation of the role of circumferential forces cause
d by interaction with the non-rotating constraint. The equations developed
suggest methods for minimizing the instability regions that are encountered
in such rotating systems when operating above their lowest critical speed.
Numerical examples are presented for the case of a rotating string to illu
strate its instability characteristics when constrained by a single degree
of freedom viscously damped system. (C) 1999 Academic Press.