>I have scratch built a 1/10th scale PSS Me109 from white foam and
>brown paper (some ply and balsa as well). Elevator and Aileron only.
[quoted text clipped - 8 lines]
>answer? Or have you any other pointers to better flying
>characteristics?
Blunt, rounded leading edges and fat airfoils are better for avoiding
snaps than sharp leading edges on thin airfoils.
Check the incidence of the wing against the incidence of the
horizontal stab. Your need for up-elevator may come from
having them working against each other.
Go ahead and try some nose weight. If it helps stabilize the
plane, that's good. Planes that are too nose heavy can often
be landed OK; planes that are tail heavy often can't.
You might want to try putting a little washout in the wing
tips or using stall strips on the inner 1/3rd of the wing.
This sometimes makes tip stall less severe because different
parts of the wing stall at different angles of attack.
Don't slow down too much on landing until you figure out
the problem. A touch plane like yours is a prime candidate
to stall, snap, and spin while attempting to land.
Marty

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markzoom@digiverse.net - 29 Apr 2007 15:59 GMT
On 29 Apr, 15:42, "Martin X. Moleski, SJ" <mole...@canisius.edu>
wrote:
> >I have scratch built a 1/10th scale PSS Me109 from white foam and
> >brown paper (some ply and balsa as well). Elevator and Aileron only.
[quoted text clipped - 33 lines]
> Big-8 newsgroups: humanities.*, misc.*, news.*, rec.*, sci.*, soc.*, talk.*
> Seehttp://www.big-8.orgfor info on how to add or remove newsgroups.
Like he said: Blunt leading edge and washout are the more forgiving.
> Hi,
>
[quoted text clipped - 14 lines]
>
> Mike
Sounds to me as if you have too much elevator throw.
Can you tell us the incidence angles of the engine, wings and tail?
Also, what is the wing loading? If you don't know that, how much does
it weigh and what is the wing area?
MJKolodziej - 29 Apr 2007 19:28 GMT
>> Hi,
>>
[quoted text clipped - 20 lines]
> what is the wing loading? If you don't know that, how much does it weigh
> and what is the wing area?
One thought: how much verticle stab. do you have? If you tried to make it
scale like it may be too little for a model.
mk
> Hi,
>
[quoted text clipped - 14 lines]
>
> Mike
Those sound like classic symptoms of a too-rearward GC.
Have you done the dive test? Assuming that you can get the thing high
enough in a steady wind, get it trimmed for a slow glide. Then nose
down into a fast glide and let go of the sticks. If it tends to zoom up
when you let go then the CG is forward. If it tends to tuck under into
a steeper dive then the CG is definitely too far back. If it stays the
same then the CG is right on the knife-edge stability point. For sport
flying, you probably want to go about 1/4 inch ahead of the neutral CG
point; if you're a hot rodder then leave it right there and learn to be
gentle with the elevator (and enjoy the flick rolls).
If you don't like the dive test, then check to see how it flies inverted
compared to upright. If you can use the same elevator trim in
canopy-down flight as canopy-up then you're definitely at the neutral CG
point. If you have to stick close to the slope this may be an easier
test to do.
The other suggestions that you've gotten will all help to tame the plane
down when you get a sudden excursion in pitch, except for reducing the
elevator throw which will compensate for the CG position somewhat.
Don't discount them, but I'd get the CG right.

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gillingw@hotmail.com - 30 Apr 2007 19:37 GMT
Thanks for the info.
Will push CG forward and check relative angles of incidence on tail
and wing.
Point about scale vertical stab being too small is very interesting.
If I re-build I will look at bigger vertical stab and enlarge the wing
tip slightly over scale.
Thanks Mike
Tim Wescott - 30 Apr 2007 19:43 GMT
> Thanks for the info.
> Will push CG forward and check relative angles of incidence on tail
[quoted text clipped - 4 lines]
>
> Thanks Mike
You can test the vertical stab notion by building a slip-on extension.
If it makes a noticeable improvement then you can think about increasing
its area (or seeing if there's a later version of the original that used
a dorsal fin).

Signature
Tim Wescott
Wescott Design Services
http://www.wescottdesign.com
Posting from Google? See http://cfaj.freeshell.org/google/
Do you need to implement control loops in software?
"Applied Control Theory for Embedded Systems" gives you just what it says.
See details at http://www.wescottdesign.com/actfes/actfes.html