Research Article
Effects of the Air Inlet Angle on the Combustion and Ablation Environment of a Hybrid Powder-Solid Ramjet
| Boundary name | Boundary type | Mass flow rate (kg/s) | Total pressure (MPa) | Total temperature (K) | Species |
| Inlet | Mass flow inlet | 0.24 | 0.5 | 1800 | 47% CO, 41% N2, 10% H2, 1% H2O, 1% CO2 | The entrance of the air inlet | Mass flow inlet | 4 | 0.5 | 573 | 21% O2, 78% N2, 1% CO2 | Outlet | Pressure outlet | 0.24 | 0.026 | 300 | — | Inner wall | No-slip wall | — | — | — | — |
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