Research Article

Influences of Tip Cooling Injection on Tip Clearance Control at Design and Off-Design Incidences

Figure 2

(a) Total pressure coefficient, (b) yaw angle, and (c) axial velocity at rotor exit, pitchwise mass-averaged.
160423.fig.002a
(a)
160423.fig.002b
(b)
160423.fig.002c
(c)