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On Mar 28, 2007, at 12:52 PM, Ernest Christley wrote:
Patrick Panzera wrote:
What's the consensus on this?
http://www.americanrotaryengine.com/id10.html
Thanks!
Pat
2.29 reduction ratio? That will limit most propeller to around 5800 RPM. That's going to leave a lot of horses corralled.
-- ,|"|"|, Ernest Christley |
----===<{{(oQo)}}>===---- Dyke Delta Builder |
o| d |o http://ernest.isa-geek.org |
Ernest, I think you are mixing engine RPM and prop RPM. I have Tracy's 2.17 reduction ratio and on takeoff the engine is running at 6,500-7000 RPM
with the IVO Magnum 68" diameter inflight adjustable . .
Buly
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