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Table 1 The flow parameters of the test cases

From: A symmetry-based length model for characterizing the hypersonic boundary layer transition on a slender cone at moderate incidence

Case

Re(×107m−1)

Ma

P0(MPa)

T0(K)

Tw(K)

AoA()

RN(mm)

GAC-0,6

0.911

7

2.288

601.4

300

0,6

1.6

CARDC-0,2,4,6

1.0

6

1.1

474

300

0,2,4,6

0.05