Hello - just discovered this gem of a project.
In one of the very well done vids of the RV4 there is mention of the system being suitable
for light straight wing prop driven aircraft.
Is there any reason it would be unsuitable for the Subsonex? Those typically use an
AOA that is derived from pitot/static as is the Gen2 so maybe a good option.
The only real bother I can see with the Subsonex is that there is significant thrust to pitch
coupling but I would expect that to be a "so what". I have been wrong before.
Thanks, and thanks very much to whomever for making this thing real and open.
B
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Yes, it will work fine.
I spent some time in a previous life working with sub-scale drones (the old-fashioned jet powered ones!) and there was always a significant pendulum effect with the pod mounted engine--they were mounted below the fuselage, so opposite of the Subsonex. There is even some effect in the 777 I fly at work. That won't effect coefficient of pressure derived alpha.