Table 6 Parameters of MF-1 flight experiment at ascent phase
From: Application of surrogate models to stability analysis and transition prediction in hypersonic flows
t/s | H/km | M∞ | Re∞/m− 1 | Tw/K | T∞/K |
|---|---|---|---|---|---|
17 | 11.20 | 4.54 | 3.333 × 107 | 518 | 216.65 |
18 | 12.24 | 4.87 | 3.036 × 107 | 531 | 216.65 |
19 | 13.35 | 5.23 | 2.739 × 107 | 575 | 216.65 |
20 | 14.50 | 5.25 | 2.295 × 107 | 595 | 216.65 |
21 | 15.63 | 5.08 | 1.860 × 107 | 595 | 216.65 |
22 | 16.71 | 4.93 | 1.524 × 107 | 600 | 216.65 |