Investigation of the Shear Flow Effect and Tip Clearance on a Low Speed Axial Flow Compressor Cascade

Figure 4

Comparison of 𝐶_𝑝 on C4 blade surface between experiment, and CFD at 𝑖=10^∘, (a) 𝑧/𝐻=50%, midspan and (b) 𝑧/𝐻=0.03, near the end wall.

(a)

(b)