Periodic flows past multiple blades and wakes aligned or nearly aligned in
the streamwise direction are studied for high Reynolds number. The interact
ion between the blade and wake sections of the flow, and the inner-outer vi
scous-inviscid interaction, lead to an elliptic problem requiring the solut
ion of the boundary-layer equations together with a pressure-displacement r
elation which extends over the whole period. This is solved computationally
, with the results showing in particular cases of boundary-layer separation
from the blades. The results also lead to an analysis for blades of short
streamwise extent compared with the inter-blade distance, an arrangement of
practical relevance to rotorcraft. Both the numerical and the analytical a
pproaches yield the result that viscous effects cause an abrupt reduction o
f pressure over the blade, balancing a gradual pressure growth throughout t
he wake.