{It seems the edit function won't let me change the
mis-spelling in the subject line even though I
was logged on.}
...or a really dumb idea? I just read the article about
the "Doctor" and am thinking about airfoils and flaps. I have a
Sig Twister which I am just beginning to build. I am planning on
lengthening the fuselage as in the Fancherized version (thanks
to everyone who responded to my previous post on that question).
The Twister has a thick airfoil (22% I believe), and I am
thinking if I built the wing making the leading edge more blunt
than shown in the plans and glued the flaps on stationary
I could get a wing *similiar* in lift characteristics to the
Doctor or Medic without the extra problems of trimming involved
with flaps.
Before responding, some background: I have been flying for only
1 year, and at this point am not looking towards flying
competitively. I am merely a sport, or "Sunday" flyer or
whatever you want to call it. But I do want to learn to fly
the full pattern. All the planes I have flown so far have
been of the "old-fashioned" style, i.e. fixed leadouts,
fixed tip weight, rudder offset, unflapped. As such, they tend to
have outward yaw. They fly *OK* but need faster lap times
than the "accepted norm." My intent was to build the Twister
with adjustable leadouts, a weight box, and no rudder offset.
After reading the "Doctor" article, I realized it might be
better to learn how to trim an unflapped plane really well
first before jumping all the way in and trying to trim a
coupled-flap stunter with all the extra variables involved.
The obvious answer is to build a Doctor or Medic, but 1) I'm
still in the kitbuilding stage & don't know if I'm ready to build
cutting all my own parts; and 2) I already have the Twister.
So what I'm wondering is do you think the Twister will
fly ok with the flaps left stationary at a 5.1 to 5.2 second
lap time? Would a blunter leading edge be of any benefit?
Or is it just a dumb idea? If so, forgive my ignorance.
Sorry for the length of this, and
thanks in advance.
Ed N.