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Canard/Elevator Issue/Problem
Issue Statement
The problem is, I seem to have somehow cut the canard with the trailing
edge (and the elevators) about 1/8" low, although I used the elevator
mounting templates when attaching the elevator hinges. Here's a
diagram of what I've got in relation to what it's supposed to look
like:
As I said, the offset is about 1/8". The canard is smooth, the airfoil
shape on the canard and the elevators match up with the templates
(except for the last 1" of the canard where it slopes down too far).
So, I had the following questions: Do I need to completely remake my
canard or the trailing edge? Do I need to remove the elevator hinges
and raise the elevator 1/8"? Or can I just leave everything the way it
is? Is there some other resolution?
Obviously, I have concern from an aerodynamic and safety standpoint, and
want to make sure that I will be able to fly safely. If it's only a
question of one or two knots in speed, I won't be concerned. If I
need to perform some major rework, of course I'll do it,
but if it's safe the way it is, I'll leave it.
Resolution Plan
After writing to Nat Puffer, Vance Atkinson, John Roncz, posting to the
COZY mailing list and
rec.aviation.homebuilt, I
received a goodly number of reasonable responses, which I will summarize
here. I'll list them in my completely subjective determination of
quality, and summarize and paraphrase:
- From Nigel Field and Nick Parkyn:
This is important - don't fly like this. Fix it by adding foam
and/or glass to the top of the trailing edge of the canard to build
it up to the correct shape. Sand away the bottom of the trailing
edge of the canard, and then re-glass to join with the new glass from
the top surface. Now, the canard is correct. Then rip out the
hinges and re-install them 1/8" further up. Then, re-do the wingtips
to match the new trailing edge and elevator.
- From John Roncz (THE MAN):
(Incidentally, I got a response from him within 24 hours - I was VERY
happy!). John said (after looking at the web page picture) that if
it was HIS plane, he'd fly it, see if it exhibited any bizarre
behavior, and then fix it if it did. He felt that it might raise the
effective angle of attack slightly (the way it is) and that the hinge
moments might increase slightly, affecting the stick forces. He
didn't think it would be significant, however. (Some other
respondents had the same basic comments).
- From Nat Puffer:
Nat didn't want to commit to what the changes might be, but suggested
building up the BOTTOM of the canard 1/8" with filler to blend into
the bottom of the elevator.
Some people suggested (and offered) to perform computer analyses of the
two different airfoils to try to predict what might happen. Given my
experience with Finite Element Analysis and Fluid Dynamics codes, I
don't think that the uncertainty involved here would tip the balance one
way or the other as far as what I should do, and would involve as much
work on the part of myself (and others) as just fixing the damn canard
:-).
So, what am I going to do?
While I'd really like to ignore it, and follow John Roncz's suggestion,
I've about run out of money for a while so I can't work on the landing
gear (the next chapter in the ad-hoc schedule). This will give me a
month or two over the winter to follow Nigel and Nick's recommendations
(and many other people's suggestions) to fix it, and NOT fly as it is,
and it'll cost less than $100 to do so.
What's an extra month over 4-5 years, when my safety's at stake, eh?
:-).
Addendum to: what am I going to do?
After more thought, and a remeasuring of the canard, I've decided to
follow John Roncz's advice and see what happens. I've had discussions
with L.E. builders who've said that they've seen any old crap that people
build get into the air, and I'm nowhere near what they described as "any
old crap". The offset measures closer to 1/16" than 1/8", after a
remeasurement. Anyway, that's the current plan.
Thanks again to everyone - I really appreciate it. I urge everyone to
check their airfoils against the templates before and after hotwiring
and sawing off the "fishtail" - had I done that, I'd have saved myself a
lot of work.
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Copyright © 1995, 1996, All Rights Reserved, Marc J. Zeitlin