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)
4E+ 6
0.1
6
5.23
0.2
13.18
0.5
44.73
1.0
112.71
2.0
284.0
5.0
963.62