Quote:
Originally Posted by Robo.
I see what he means now, thank you. It doesn't make much sense though - engines are designed for certain HP and that was never achieved at max. continuous rating as far I can tell.
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Rolls Royce gives 990 b.h.p as "international power rating" (+ 6 1/4 Boost with 2,600 RPM at 12,250 feet), see
http://forum.1cpublishing.eu/attachm...8&d=1334724563.
Don't we have to convert the boost values to ata before we compare them make a statement about the factor between them? Otherwise the atmospheric pressure offset is not eliminated.