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

Figure 3

Resulting GCI error band from the mesh sensitivity analysis for the profiles of the velocity magnitude in plane 𝑥𝑦, 𝐶_𝑥𝑦=(𝑈²+𝑉²)^0.5, extracted at 𝑦=−132, 𝑥=300 mm (a) and 𝑦=−132, 𝑧=0 mm (b), respectively.

(a)

(b)