my view is based on using the performance in a 1 atmosphere environment (aka sea level) Fig 7ringo wrote: Well, i'm very quiet on this, reason being i'm very cautious about apply those figures to an automotive engine and expect similar results. The aircraft operates in a very low pressure environment, with very low temperatures, maybe below zero at altitude and possibly steady speed. I wouldn't be so keen to apply the figures to a car that runs in a 1 atmosphere environment at normal temperatures.
it shows the value of - delta P of 20" Hg in maximising efficiency in this case
that's a difference in mean pressure across the turbine of 1 bar
in F1 this would be close to 2 bar, that alone should generate decent power
that's why the max efficiency delta P is greater (more negative) at greater ambient pressures
that's how power migrates from crankshaft to turbine