From: Experimental study of bluntness effects on hypersonic boundary-layer transition over a slender cone using surface mounted pressure sensors
Reunit (1/m)
R (mm)
Ma
xsw (mm)
10E+ 6
0.1
6
7.10
0.2
17.89
0.5
60.70
1.0
152.96
2.0
385.45
5.0
1307.83