aircraft:tmd:turbo_engines
Differences
This shows you the differences between two versions of the page.
| Both sides previous revisionPrevious revision | Last revisionBoth sides next revision | ||
| aircraft:tmd:turbo_engines [2021/02/12 13:14] – [Step 6 - Engine control (FADEC)] jh | aircraft:tmd:turbo_engines [2021/02/12 13:51] – [Step 6 - Engine control (FADEC)] jh | ||
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| Line 457: | Line 457: | ||
| Enrichment = Engine1Station3.OutputTotalPressure / ( PitotTube.StaticPressure * DesignCompressionRatio ). | Enrichment = Engine1Station3.OutputTotalPressure / ( PitotTube.StaticPressure * DesignCompressionRatio ). | ||
| - | FuelFlowRaw = C_FF * ( Governor + Enrichment ) | + | Gain = PitotTube.StaticPressure / 101325.0 |
| + | |||
| + | FuelFlowRaw = Gain * C_FF * ( Governor + Enrichment ) | ||
| FuelFlow = clamp( FuelFlowRaw, | FuelFlow = clamp( FuelFlowRaw, | ||
aircraft/tmd/turbo_engines.txt · Last modified: 2022/08/02 10:00 by jh