In the present experimental study, the effect of blade number, nozzle
entry are, and head on the performance characteristics of a cross-now
turbine have been investigated. It has been observed that the efficien
cy of the turbine increases with increase in blade number, nozzle entr
y are, and head. The present investigation has also shown that there i
s an optimum number of blades for a given nozzle entry are beyond whic
h the performance of the cross-flow turbine deteriorates. It has also
been shown that cross-now turbines at higher heads do not behave as pu
re impulse turbines.