Research Article
Experimental Study on Aerodynamic Heating Induced by Dual Injections into Hypersonic Cross Flow
Table 1
Test flow parameters.
| Mach number, | Total pressure, | Static pressure, | Total temperature, | Re |
| 8.1 | 4.0 [MPa] | 377 [Pa] | 876 [K] | 6.5 Ć 106 [mā1] |
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