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Well folks, I hope I'm not opening up a can of worms on this. I searched
the usenet archives on google about this, and nothing quite answered my question, so... I emailed Skystar, but want to ask here too. The kit manufacturer claims a 150mph cruise and 160mph top speed. This seems a little optimistic. This is a side-by-side 2 seater, 100-115hp engine (turbo maintains output to 16,000 feet), approx 1500lbs gross weight (about 750 empty). The 100hp normally aspirated engines list 120 and 125mph for cruise and max respectively. So it doesn't quite add up... Has anyone backed this up in practice? I did some rough calculations on scratch paper. The short answer is it _might_ be possible. Taking into account the turbo engine's higher output at high altitude, and that the non-turbo aircraft probably max out TAS at about 5,000ft compared to over 10,000 for the turbo, air density's effect on profile drag vs induced drag, air density effect on the normally aspirated engines... Again, my best answer is... maybe. Thanks for any help. |
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