Periodic Inversion is a new approach for the calculation of rotor free
wakes which solves directly for periodically steady-state solutions,
at all advance ratios including low speed and hover. This is a unique
capability as traditional time marching solutions can fail to converge
at low advance ratios. The method is based on enforcing a periodic bo
undary condition on the wake over one rotor revolution. The resulting
system of nonlinear equations is linearized, then iteratively solved f
or perturbative corrections to the wake geometry. The method is used t
o examine the low speed wake structure, which exhibits three distinct
forms depending on advance ratio: a helical structure from hover to so
me lower bound advance ratio, a roll-up structure above some higher bo
und advance ratio, and a rapid transition region between the two. Perf
ormance curves are generated by varying trim parameters between iterat
ions.