I am researching the Merlin 266 in combination with the Spitfire Mk.XVI. When checking the internet or books, the only mention ever made is that it is sort of a carbon copy of the Merlin 66, but built by Packard and with the same performance.
It does however have a few differences:
1. Reduction Ratio of 0.479 (in stead of the 66's 0.477)
2. Supercharger Gear Change altitudes MS > FS @ 11,000ft & FS > MS @ 10,000ft (in stead of 66 : 14,000ft & 12,500ft)
I would like to know the reasons of this and am also wondering if there are any performance trial data around, like graphs or tables?
Thanks
It does however have a few differences:
1. Reduction Ratio of 0.479 (in stead of the 66's 0.477)
2. Supercharger Gear Change altitudes MS > FS @ 11,000ft & FS > MS @ 10,000ft (in stead of 66 : 14,000ft & 12,500ft)
I would like to know the reasons of this and am also wondering if there are any performance trial data around, like graphs or tables?
Thanks