The analysis of the self-induced velocity of a single helical vortex (Boers
ma & Wood 1999) is extended to include equally spaced multiple vortices. Th
is arrangement approximates the tip vortices in the far wake of multi-blade
d wind turbines, propellers, or rotors in ascending, descending, or hoverin
g flight. The problem is reduced to finding, from the Biot-Savart law, the
additional velocity of a helix due to an identical helix displaced azimutha
lly. The resulting Biot-Savart integral is further reduced to a Mellin-Barn
es integral representation which allows the asymptotic expansions to be det
ermined for small and for large pitch. The Biot-Savart integral is also eva
luated numerically for a total of two, three and four vortices over a range
of pitch values. The previous finding that the self-induced velocity at sm
all pitch is dominated by a term inversely proportional to the pitch carrie
s over to multiple vortices. It is shown that a far wake dominated by helic
al tip vortices is consistent with the one-dimensional representation that
leads to the Betz limit on the power output of wind turbines. The small-pit
ch approximation then allows the determination of the blade's bound vortici
ty for optimum power extraction. The present analysis is shown to give reas
onable estimates for the vortex circulation in experiments using a single h
overing rotor and a four-bladed propeller.