A mathematical model has been created for complex simulation of the process
of blade surface formation in unsteady mode. It is based on the assumption
s of the one-dimensional theory in the feather regions of blade and the ass
umptions of two-dimensional electrostatic field in the edges vicinities. La
place equation is solved by panel method. One-dimensional unsteady transfer
equations are solved along edges by finite difference method. (C) 2001 Pub
lished by Elsevier Science B.V.