ORIGINAL: Commander Stormwolf
turbos and multi-stage superchargers will allow the engine to maintain power
to high altitudes - where there is less air resistance, that is why the top speed is high at high altitudes
at low altitudes, the system is useless weight and drag, and decreases the top speed of an identical plane
that would be single-stage supercharged
I am not sure what you are referring to .. but ... for example .. the TSIO-360-MB develops 4" greater manifold pressure all the way to the crtical altitude of 18000 feet the TSIO-420-N develops this all the way to 27,000 feet. In these cases more power than an normally aspirated engine by increasing the virtual stroke volume.
(CI * LS * RPM) /K = HP .. cubic inches * linear stroke * RPM / constant = Thrust HP * efficiency = BHP brake horsepower ..
It is quite possible to produce a heck of lot more HP for much less weight by increasing the stroke volume above normal atmosphere right up to the critical altitude.. it was the Mooney Mantra ..and how the Bravo was the fastest single in the business
The problem is heat .. it is explained in my article ..




