I have had my glider plans for approximatly 9 years now.
My question is, does anyone know the Airfoil used by the Woodstock
Glider?
NACA ###?
Thanks
Herbie
> NACA ###?
More likely Culver ####.
Ah, here it is: Culver 18%:
http://www.ae.uiuc.edu/m-selig/ads/aircraft.html
More than likely, the 18% is the thickness (T/C), nice and deep to
keep the spar simple and cheap.
Who's Irv Culver? Just the guy who was at the center of the design of
some of the hottest airplanes of the 20th century. The guy who gave
Kelly Johnson's "Skunk Works (R)" its name.
http://www.ssa.org/myhome.asp?mbr=5811273455&show=blog&archive=9/1/1999
http://www.lockheedmartin.com/aeronautics/skunkworks/name.html
Thanks, Bob K.
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Regards,
Doug
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Correct me if I'm wrong, but there is no washout in this design is
there?
Sorry, yet another question, are the Airfoil Data points freely
available?
> Correct me if I'm wrong, but there is no washout in this design is
> there?
If there is, it will be shown in the plans. It might also be covered
in _Fundamentals of Sailplane Design_, but my copy is not handy.
> Sorry, yet another question, are the Airfoil Data points freely
> available?
Probably not. It's not at the UIUC site, so it's probably not freely
available. From what I've heard, it was a one-off profile (OK, two-off
if you count the substantial difference between the root and tip
shapes) that Irv did on a relatively casual basis.
Thanks, Bob K.
I'm looking at the plans, and there is no Washout, that I can detect,
which is why I'm asking.
The spar cutouts are exactly the same relative position on all the
foil profiles, with no twisting.
I am also an Aerospace Engineer, been working mostly mechanical for
the last 8 years so my aerospace brain has cobwebs, but I do know how
to read a drawing, my guess is it was this way for ease of
construction.
I'll re-read the assembly manual again.
I scanned sheet one of the 13M drawings and have the foils now in a
DWG format.
What I'll do is use Pro/E to loft between foil 1 and 20, then insert
each foil from 1 to 20 at station, then generate cross sections at
each station to see if they all meet up.
Herbie.
Yup, that's the way I understand it - there's no angular difference
between the chord lines of the root and tip sections, but the profile
differences between the root and tip airfoils make the wing act as if
there are.
Here's a couple of pictures from the Les Sparks site that shows the
Woodstock wing profiles:
http://members.aol.com/lessparks/clint20.jpg
http://members.aol.com/woodglider/clint25t.jpg
It's kind of hard to see in the photos, but if you look closely you
can see that the profile goes from sort of flat-bottomed at the tip to
a deeper-bellied (for lack of a better term) section at the root.
Here's the home page for the site those photos are from:
http://members.aol.com/woodglider/index.htm
I haven't heard from Les for a while, I wonder what's up with his
project.
> I scanned sheet one of the 13M drawings and have the foils
> now in a DWG format.
> What I'll do is use Pro/E to loft between foil 1 and 20, then insert
> each foil from 1 to 20 at station, then generate cross sections at
> each station to see if they all meet up.
That sounds like a good plan, that ought to work great. The main
gotcha, and you've probably already thought of this, is that old
blueprints tend to shrink and warp a bit as they age. Also, sometimes
scanners add their own scaling errors. So its possible to accumulate a
bunch of little errors that add up to something substantial. The plans
probably have some key dimensions that you can use to correct the
scaling of your DWGs; if you keep an eye on them you'll be fine.
Thanks, Bob K.
http://www.hpaircraft.com/hp-24
The original 12-meter Woodstock wing has no twist. Irv Culver
(Lockheed Skunkworks) did the airfoils at the request of designer Jim
Maupin (both now no longer with us, regrettably). Wingtip/aileron
stall protection was secured via reducing the percent section near the
wingtip. It's in the manual. Woodstock wing stall characteristics (at
least for the original 12 meter wing, which I built and flew) were
absolutely delightful: first time I stalled my n20609, on her maiden
flight, I broke out loud laughing. Perfect stall behavior; as mannerly
as it is possible to be. Despite low wing loading, the Woodstock
feels as much like Libelle as it does a SGS1-26. Easier to keep
rightside up in turbulence than a 1-26 in turbulence to boot,
particularly on aerotow.
Safe soaring,
Bob Wander
>
> That sounds like a good plan, that ought to work great. The main
> gotcha, and you've probably already thought of this, is that old
> blueprints tend to shrink and warp a bit as they age. Also, sometimes
> scanners add their own scaling errors. So its possible to accumulate a
> bunch of little errors that add up to something substantial. The plans
> probably have some key dimensions that you can use to correct the
> scaling of your DWGs; if you keep an eye on them you'll be fine.
Yes, Hence me looking for data points. The chord at root and tip are
known and have hard dimensions for.
I can check that with % chord at root and tip for scaling in that
direction, print off and check over the actual prints I have.
I can also CNC Route some "test ribs" using my CNC router.