Research Article
Experimental and Numerical Investigations on the Ignition of RBCC Gas-Oxygen/Kerosene Rocket Ejector
Table 3
Numerical inlet conditions.
| | (g/s) | (m/s) | (m/s) | (m/s) | (MPa) |
| | GOX | 22.92 | — | — | — | 2 | | Kerosene inlet 1 | 3.47 | 13.06 | 0 | 22.54 | — | | Kerosene inlet 2 | 3.47 | 13.06 | 19.52 | -11.27 | — | | Kerosene inlet 3 | 3.47 | 13.06 | -19.52 | -11.27 | — |
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