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

Figure 11

Contours of the in plane velocity modulus 𝐶_𝑥𝑦=(𝑈²+𝑉²)^0.5 and stream tracers in planes 𝑥𝑦 (a–c) and 𝑥𝑦 (d–f) for Ro=0 (a, d), Ro=0.23 (b, e), and Ro=0.46 (c, f). Channel configuration 𝛾=0^∘.

(a)

(b)

(c)

(d)

(e)

(f)