Effects of Rotation at Different Channel Orientations on the Flow Field inside a Trailing Edge Internal Cooling Channel

Figure 13

Contours of 𝑈 velocity component and stream tracers at the channel inlet, 𝑥=−69.8mm, for Ro=0.46 and 𝛾=22.5^∘ (a) and 𝛾=45^∘ (b).

(a)

(b)