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Table 2 Cross-correlation of the first four PCB sensors, Reunit = 6E+ 6/m

From: Experimental study of bluntness effects on hypersonic boundary-layer transition over a slender cone using surface mounted pressure sensors

 

NO. 1 → NO. 2

NO. 2 → NO. 3

NO. 3 → NO. 4

NO. 4 → NO. 5

Δx (mm)

25

25

25

30

Δt (μs)

32.3

33.3

32.7

40.3

U/Ue

0.87

0.84

0.86

0.86