at the entrance to the nozzle
at the throat of the nozzle
in the convergent portion of the nozzle
in the divergent portion of the nozzle
Agree
Disagree
Correct
Incorrect
simple impulse turbine
simple reaction turbine
impulse-reaction turbine
none of these
blades are equiangular
blade velocity coefficient is unity
blades are equiangular and frictionless
blade solidity is 0.65