Nup ... sorry , just me being left handed .. its a standard 'TriQ' .., Graham

Graham is this a TriQ or is it something different and hence the reversed designation?

Well, that's certainly something to chew on. I have actually skimmed this before, but obviously didn't get enough out of it to understand that flying with what seem like "dirty" wings can actually

If you really want to dig into this. I have done a three part modeling study on the subject and all of the terms are defined and analyzed. I did not delve heavily into the topic of using reflexor to

Man I really seem to have opened up the tin with this one....lol

I'm getting a little confused here. I swear I'm reading conflicting info. When you reflex up, the trailing edge of the ailerons point up, correct? This produces a nose up tendency and is used on

So with these reports, I'm not sure if I would connect the the reflexor to the autopilot system. But an electric trim still sounds like a viable idea, with a joystick utilizing some buttons for trim

Sam, I have a Completed Q-Tri .. less engine and interior .. it has the Mag's cut out into the Firewall . I imported this airframe from Mike Evens in California six yrs ago . Its in my

To all the flyers, I created a listing in the database section of this Q-List. I wanted to have some kind of organized place where we can see who has actually flown their project. If this includes

My elevators fair in high speed as well. I did add 1 degree in the LS1 canard when installed. The Reflexor does not have to be used, it just refines the controls. It does however add a couple knots if

One of the QAC newsletters indicated that the factory recommended increasing the angle of the canard 1 degree for all new construction. This was recommended for the GU canard, but was issued about the

When I first started my flight testing way back in 1986, I could tell that something was wrong with my angle of incidence between the front and rear wings. So what I did, was to raise the front of the

I see the same phenomenon as Mike reports. This is the result of minimizing the overall induced drag for both wings while still providing the necessary lift for level flight. At high cruise at

This is very interesting. Does this suggest a change to the angle of incidence for one or both wings? Does it suggest a thinner airfoil? Maybe a C.G. shift? Is there precedence for flying faster (when

Can't*

I'm sure that would handle the physical aspect of manipulating the control. But the issue... And what sparked my interest in the idea, is that reflexor is pretty freaking limited in it's use in

Eugen, That is the correct stuff. -- -MD #2827 (still thinking about planning on visualizing how to finish building)

I found a small throw linear actuator that drives .75" with 30 ft/lbs of force. Does not move or freespin if power is lost. I think it weights 12oz?

There are many systems for Reflexor. My control for it takes more pressure than I'd expect a servo to handle. I also don't see it as a good elevator control. For instance, in flight I like to

What's the approximate linear throw of that mod?