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
30
Δt (μs)
32.3
33.3
32.7
40.3
U/Ue
0.87
0.84
0.86