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

Figure 15

Contours of the in plane velocity modulus 𝐶_𝑥𝑦=(𝑈²+𝑉²)^0.5 and stream tracers in planes 𝑥𝑦₁ (a, d), 𝑥𝑦 (b, e), and 𝑥𝑦₂ (c, f) for Ro=0.46, 𝛾=22.5^∘ (a–c), and 𝛾=45^∘(d–f).

(a)

(b)

(c)

(d)

(e)

(f)