I updated my website
http://www.ductedfan.com
Added a link for VTOL canard, that shows my earlier concept, and
yours, and a link to your page.
I'm going to see if I can find an x-plane model of a tail-sitter that
can be modified into something more like what you came up with.
I ran some simulations on a 12 foot 4-blade (2 one way, 2 the other
way) propeller operating at 1200 RPM
pitch HP static thrust
50 233 1864 at sea level
55 275 2090 at sea level
60 320 2320 at sea level
60 240 1712 at 10,000 feet
Assumes a two seater with gross weight around 2000 lbs.
Looks like we might need more installed HP to make sure we can always
have more than 1:1 thrust to weight under all conditions, including
takeoff from 10,000 feet. Not a problem with turbo charging. I'm thinking
no installed conventional landing gear to save weight, no wheels at all.
If the engine fails you can use helicopter mode to slow the descent. If
for some reason that doesn't work, as in loss of control of the rotor
blades, you can blow a chute out the back and come down "upside down".
Perry Mick
The Rotary Engine NewsLetter. Powered by Linux.
ACRE NL web site.
http://www.rotaryeng.net
Copyright 1998-2006 All world wide rights reserved.