[NSRCA-discussion] Fwd: RE: Design Question

Tue Nov 10 14:54:12 AKST 2009

Hi Tom.
"have a read of his (Bryan's) article". Where can I find this? I am very
interested.
Jim

-----Original Message-----
From: nsrca-discussion-bounces at lists.nsrca.org
[mailto:nsrca-discussion-bounces at lists.nsrca.org]On Behalf Of Koenig, Tom
Sent: Tuesday, November 10, 2009 1:13 PM
To: 'General pattern discussion'
Subject: Re: [NSRCA-discussion] Fwd: RE: Design Question

Hi Jim and all,

Jim.....enjoy those long winters, have a hot cup of coffee....and realy, I
mean really, think about what Bryan tells you. It is a brain twister and can
be confusing. But...he is right in everything he tells you. I realise there
are people out there who do not agree with Bryan, and that is fine, but my
advice is to have a read of his article-if only for interest.

If I had the time, and my ability to express myself were better-I would try
to explain some of my design ideas. But I simply suck at that-hence my
initial response, just go for it.

Another genius to ask(besides Bryan) would be Nat Penton...he will also make
your head spin! A very learn'ed man indeed.

Draw a line on a sheet of paper as your Datum, mark out 2 meters and go for
it. Better still, use some CAD package.

PS. Make it pretty-or you wont want to fly it!! Also-keep us informed how
you are going. I certainly am interested in your project, maybe others are
too.

Tom

-----Original Message-----
From: nsrca-discussion-bounces at lists.nsrca.org
[mailto:nsrca-discussion-bounces at lists.nsrca.org] On Behalf Of
shinden1 at cox.net
Sent: Wednesday, 11 November 2009 7:48 AM
To: General pattern discussion
Subject: Re: [NSRCA-discussion] Fwd: RE: Design Question

Ok
Bryan
---- shinden1 at cox.net wrote:
>
> > From: "J N Hiller" <jnhiller at earthlink.net>
> > To: <shinden1 at cox.net>
> > Subject: RE: [NSRCA-discussion] Design Question
> > Date: Tue, 10 Nov 2009 09:51:44 -0800
> >
> > Bryan, I find it hard to believe that vertical wing placement doesn't
affect pitch trim. The wing especially a thick one contributes significantly
to total drag and any offset between the center of drag and center of thrust
would create a rotational moment that would need to be balanced with H-stab
/ elevator trim. Maybe it's insignificant compared to other factors. This is
what I'm trying to understand.
> > Yes CG is a significant contributor. I've been able to change vertical
pitch by changing the CG and wing incidence, forcing a H-stab / elevator
trim change. CG placement is a whole different issue as is weight in the
extremities such as wing tips, nose and tail.
> > Thanks.
> > I'm really interested in this aspect of pattern, good thing, winters are
long here.
> > Jim
> >
> > -----Original Message-----
> > From: shinden1 at cox.net [mailto:shinden1 at cox.net]
> > Sent: Monday, November 09, 2009 7:14 PM
> > To: General pattern discussion
> > Cc: J N Hiller
> > Subject: Re: [NSRCA-discussion] Design Question
> >
> > Hi Jim
> > The vertical wing placement has no effect on pitch trim,,NONE !
> > what does is,the incidence and C/g. Don`t even worry about it.
> > However it will effect  Dihedra you will need to move the wing after the
test flights. or rebuild a new one with the right dihedral or, Mix it out.
> > Rudder angles ,sweep, or position ,has a tiny effect ,so little it`s not
worth worrying about .draw something that looks good.
> > Just build your airplane and adjust to what it does not do well.
> > your not going to hit it on the first try,but the effort will be worth
the Learning and enjoyment, in a self designed model.
> > There are so many dynamics involved in designing your first airplane
> > you cant possibly think of them all on the first attempt.
> > just  have fun and build a light pretty model.
> > Bryan
> > ---- J N Hiller <jnhiller at earthlink.net> wrote:
> > > Thanks Lance. I don't want to stray too far from proven relationships
but
> > > understand there are many variables rendering each design different.
> > > I presently have the wing located 1/2" below a centerline through the
H-stab
> > > and engine centerline. The stab is about 1/2" above the tail tube
centerline
> > > and positioned about 1/4 the height of the V-stab.
> > > Both the wing and stab will be adjustable and previsions are included
for
> > > changing thrust angles. Tweaking these angles should effectively
change the
> > > flying height of the tail but the wing offset remains about the same.
> > > Other than changing the vertical center of drag what are the pros and
cons
> > > associated with positioning the wing higher or lower. I'm thinking the
> > > vertical center of drag relative to the thrust line can contribute
> > > significantly to pitch trim. Is it a major influence?
> > > Before beginning to cut parts it occurred to me that the design /
> > > construction detail offers considerable leeway in vertical wing
placement,
> > > maybe as much as an inch higher or lower from the -1/2 presently
planned and
> > > changing the wing location later will require major surgery.
> > > I guess what I'm really looking for is more understanding of the
effect
> > > vertical wing placement has on pitch trim. I guess I asked the wrong
> > > question. Any thoughts on this will be helpful.
> > > Thanks
> > > Jim
> > >
> > > -----Original Message-----
> > > From: nsrca-discussion-bounces at lists.nsrca.org
> > > [mailto:nsrca-discussion-bounces at lists.nsrca.org]On Behalf Of
> > > patterndude at tx.rr.com
> > > Sent: Monday, November 09, 2009 2:38 PM
> > > To: General pattern discussion
> > > Subject: Re: [NSRCA-discussion] Design Question
> > >
> > > That's all?  There a number of design issues we face in pattern where
> > > there's little documentation readily available. This is one, KE flight
is
> > > another, wing incidence and engine thrustline effects in 4 axis flight
is
> > > another. The more I think about it the more I think of.
> > >   There's no one answer and anything between the chordline and
thrustline
> > > can be made to work by changing rudder shape and incidence. I settled
on a
> > > quarter inch above the chordline and then adjusted the rudder to allow
a
> > > trim incidence near zero so inverted flight is more effortless.
> > >
> > > Lance
> > > AeroSlave
> > > Sent via BlackBerry by AT&T
> > >
> > > -----Original Message-----
> > > From: "J N Hiller" <jnhiller at earthlink.net>
> > > Date: Mon, 9 Nov 2009 09:36:13
> > > To: NSRCA Mailing List<nsrca-discussion at lists.nsrca.org>
> > > Subject: [NSRCA-discussion] Design Question
> > >
> > > Hello all.
> > > Here's a topic for discussion that I'm personally very interested in
and may
> > > be of interest to others.
> > > I'm working up a new pattern design and would appreciate comments
regarding
> > > the vertical placement of the wing and thrust line relative to the
stab
> > > centerline.
> > > I not only would like to know what the vertical offset is on modern
pattern
> > > designs but how the vertical location affects flight trim, and why?
> > > Thanks all.
> > > Jim Hiller
> > >
> > >
> > >
> > > _______________________________________________
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>
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