Fig. 16
Distribution of relative flow angles in the rotor reference frame. (a) (z, θ) plane at r* = 0.96, (b) and (c) θ1, θ2 planes when the θ2 plane is at s/c = 0. Insert in (b) shows the relative flow angle in θ1 for the untreated case.
Distribution of relative flow angles in the rotor reference frame. (a) (z, θ) plane at r* = 0.96, (b) and (c) θ1, θ2 planes when the θ2 plane is at s/c = 0. Insert in (b) shows the relative flow angle in θ1 for the untreated case.
