The flowfield around a gust generator device, an airfoil/rotating slot
ted cylinder (RSC) system, is numerically simulated using the general-
purpose finite element program FIDAP. The how is assumed to be quasist
eady, turbulent, incompressible, and two dimensional, The turbulence i
s modeled far from the walls by a high Reynolds number k-epsilon model
. In the near-wall region, which includes the viscous sublayer, the mi
xing length concept is used to model turbulence, The numerical analysi
s treats the time-varying flow around the gust generator device as qua
sisteady and solves the flow position by-position as the RSC rotates.
The variation of lift and drag as a function of the rotation angle and
as a function of the gap between the airfoil and the rotating slotted
cylinder is calculated.