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

Figure 10

Contours of 𝑈 velocity component and stream tracers at the channel inlet, 𝑥=−69.8mm, Ro=0 (a), Ro=0.23 (b), and Ro=0.46 (c).

(a)

(b)

(c)