NUMERICAL-CALCULATION OF FLUTTER DERIVATIVES VIA INDICIAL FUNCTIONS

The central focus of the present study is the numerical calculation of flutter derivatives. These aeroelastic coefficients play an important role in determining stability, or rather, instability of long, flexib le structures under ambient wind loading. In recent years, the Finite Element Method (FEM) has gained considerable acceptance in the solutio n of problems governed by the viscous, incompressible flow equations. FIDAP is one such general fluid dynamics analysis package that makes u se of Finite Element methodology. The most direct way of obtaining flu tter derivatives would be to simulate the full oscillatory object moti on in a flow and use the unsteady lift and moment forces thus determin ed. This would essentially entail an internal boundary motion in the f low, which requires considerable computational effort in the case of m ost Eulerian non-adaptive grid-based numerical methods. However, the a lternative indicial function approach investigated in this study limit s itself to step changes in motional variables. Inherent to using this approach, then, is the assumption of reduced computational complexity . (C) 1996 Academic Press Limited