Open Access
Table 1
Values of the design point of the studied engine.
| Parameter | Value |
|---|---|
| Bypass ratio | 5.5 |
| Overall pressure ratio | 34 |
| Max. thrust (kN) | 134 |
| Inlet air mass flow (kg/s) | 427 |
| Fuel mass flow (kg/s) | 1.307 |
| Inlet HPT temperature (K) | 1580 |
| LPS & HPS speeds (rpm) | 5000, 14460 |
| Mach, Altitude | 0, 0 |
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