Advances in Aerodynamics

Table 1 The coordinates of probe points in the Group 1 (upstream of the transition front) and Group 2 (downstream of the transition front)

From: Wall pressure beneath a transitional hypersonic boundary layer over an inclined straight circular cone

Group 1	A	B	C	D	E	F	G	H
x (mm)	220	260	300	340	450	500	600	650
θ (^∘)	75.7	94.3	109.4	115.8	132.3	143.3	155.5	174.7
Group 2	A’	B’	C’	D’	E’	F’
x (mm)	280	320	360	400	500	600
θ (^∘)	60	80	98	105	123	130

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