Table 2 Operation conditions on the DLR combustor
Case | Air pressure [MPa] | Air Temperature [K] | Burner air flow [g/s] | Cooling air flow [g/s] | Fuel flow [g/s] |
|---|---|---|---|---|---|
Isothermal | 0.4 | 295 | 82 | 0 | 0 |
Reactive | 1.0 | 650 | 140 | 39 | 6.8 |
Case | Air pressure [MPa] | Air Temperature [K] | Burner air flow [g/s] | Cooling air flow [g/s] | Fuel flow [g/s] |
|---|---|---|---|---|---|
Isothermal | 0.4 | 295 | 82 | 0 | 0 |
Reactive | 1.0 | 650 | 140 | 39 | 6.8 |