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Land Shorter VG's on Firestar II
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pj.ladd(at)btinternet.com
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PostPosted: Tue Mar 28, 2006 5:48 am    Post subject: Land Shorter VG's on Firestar II Reply with quote

Did I hear someone call for a wind tunnel....?>>

Hey, thats great. Can you do smoke or tufts? Pics would be nice but that is
asking a bit much.

The position that I am desperately trying to defend here is my contention
that the tail plane alone does not exert lift. When the elevator is applied
the tail plane/elevator combination DOES assume a rough airofoil shape and
consequently produces some lift.
In that case with VG`s on the underside of the tailplane and the elevator in
the `up` position they would do exactly what they do on the top of a wing.
Keep the boundary layer from breaking away. That would increase the
effectiveness of the `up` elevator.

Can you prove or disprove?

Cheers

Pat

do not archive

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John Jung



Joined: 10 Jan 2006
Posts: 108
Location: Surprise, AZ, USA

PostPosted: Tue Mar 28, 2006 6:38 am    Post subject: Re: Land Shorter VG's on Firestar II Reply with quote

Group,

I tried a couple of times yesterday to get to talk to Joa from Landshorter. I also e-mailed him with a copy of Chris Mallory's post, so that he could confirm or correct. I will report to the list after I hear from him.

do not archive


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John Jung
Firestar II N6163J
Surprise, AZ
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John Jung



Joined: 10 Jan 2006
Posts: 108
Location: Surprise, AZ, USA

PostPosted: Tue Mar 28, 2006 6:54 am    Post subject: Re: Land Shorter VG's on Firestar II Reply with quote

Group,

Joa did respond to the list last night. I should read everything before I reply to anything in the morning. He changed the subject line.

Anyway, what he accomplished with VGs on the underside of the horizontal stab is exactly the way my Firestar II flys now. So adding them to my stab would be a waste of time and money.


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Firestar II N6163J
Surprise, AZ
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Richard Pike



Joined: 09 Jan 2006
Posts: 1671
Location: Blountville, Tennessee

PostPosted: Tue Mar 28, 2006 6:55 am    Post subject: Land Shorter VG's on Firestar II Reply with quote

Instead of agreeing with or denying your position, let me simply muddy
the waters:
For the last couple years I have been designing and building radio
control airplanes out of fan fold insulating foam and typically I have
given all of them a very thick airfoil because it makes it easier to
build a light wing, plus creates other good flying attributes. Lately I
have gone the opposite direction and currently have two airplanes that
have only a flat sheet wing, reinforced by a carbon fiber tube as a main
spar. And they fly just as good as the ones with a real airfoil.
Obviously we are talking very light wing loadings here, but in certain
applications, a flat surface produces all the lift you need. I attached
some pics, maybe they will go through.

In the case of a Kolb, we have several degrees of incidence between the
wing and the tail, and if the airplane is properly trimmed, the elevator
will be exactly aligned with the horizontal stab while in flight, and
this will be providing the proper downforce to balance the center of
lift of the wing with the thrust and load of the wing. And if the
elevator/stab is providing downforce when undeflected, then...?
(And it must of necessity be creating downforce, due to the decalage
between the wing and the tail. Also, I strongly doubt that the center of
lift of the Kolb airfoil would ever match the center of gravity of the
airplane. Because if it would, then no decalage between the wing and
tail would be necessary. Of course, it would make for a very unpleasant
to fly, generally unstable airplane)

Richard Pike
MKIII N420P (420ldPoops)
pat ladd wrote:
Quote:


Did I hear someone call for a wind tunnel....?>>

Hey, thats great. Can you do smoke or tufts? Pics would be nice but that is
asking a bit much.

The position that I am desperately trying to defend here is my contention
that the tail plane alone does not exert lift. When the elevator is applied
the tail plane/elevator combination DOES assume a rough airofoil shape and
consequently produces some lift.
In that case with VG`s on the underside of the tailplane and the elevator in
the `up` position they would do exactly what they do on the top of a wing.
Keep the boundary layer from breaking away. That would increase the
effectiveness of the `up` elevator.

Can you prove or disprove?

Cheers

Pat

do not archive




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Kingsport, TN 3TN0

Forgiving is tough, being forgiven is wonderful, and God's grace really is amazing.
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n79rt(at)kilocharlie.us
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PostPosted: Tue Mar 28, 2006 12:16 pm    Post subject: Land Shorter VG's on Firestar II Reply with quote

The position that I am desperately trying to defend here is my
contention
that the tail plane alone does not exert lift. When the elevator is
applied
the tail plane/elevator combination DOES assume a rough airofoil shape
and
consequently produces some lift.
In that case with VG`s on the underside of the tailplane and the
elevator in
the `up` position they would do exactly what they do on the top of a
wing.
Keep the boundary layer from breaking away. That would increase the
effectiveness of the `up` elevator.

Can you prove or disprove?

Cheers

Pat

<snip>
OK Pat...I'll answer your question with another question...if a "flat"
surface can't generate lift then how the heck did the Concorde ever fly?
(Or the Mirage, or F-102 Delta Dart)

Point being anything that can deflect air one way will produce lift (or
just call it FORCE) the other way...it's that old "For every action
there is an equal and opposite REACTION" thing...Newton wasn't it?

Jeremy


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beauford(at)tampabay.rr.c
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PostPosted: Tue Mar 28, 2006 5:16 pm    Post subject: Land Shorter VG's on Firestar II Reply with quote

Brother Patrick...
Prove...? Disprove...? Lift...? Your induced-airfoil theory makes
intuitive sense to me...

But, nossir, I can only offer my empirical before and after
impressions... flare the little airplane
down in ground effect, power off, with my flabby butt strapped in the
pointy end, and there is a markedly
reduced tendency to perform a soil-sampling drill when the VG's are
installed on the bottom of the
tail...

Per your inquiries... Smoke is available if you furnish the
Macanudo... I no longer do tufts... it's a
matter of principle, Sir... Pictures are most assuredly out of the
question... we have our standards....

Beauford of Brandon
FF#076
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Russ Kinne



Joined: 27 Jan 2006
Posts: 182

PostPosted: Tue Mar 28, 2006 6:16 pm    Post subject: Land Shorter VG's on Firestar II Reply with quote

Pat
As I understand it, the tailplane does create "lift", but in an
upward direction -- because it is behind the CG.
In effect, it keeps the tail DOWN. Which is why it's basically an
upside-down wing, and the VG's should be on the underside.
I think your contention is wrong, desperate or not. but I could be
wrong; that happened once. Or twice.
Best,
Russ
do not archive
On Mar 28, 2006, at 8:43 AM, pat ladd wrote:

Quote:


Did I hear someone call for a wind tunnel....?>>

Hey, thats great. Can you do smoke or tufts? Pics would be nice but
that is
asking a bit much.

The position that I am desperately trying to defend here is my
contention
that the tail plane alone does not exert lift. When the elevator is
applied
the tail plane/elevator combination DOES assume a rough airofoil
shape and
consequently produces some lift.
In that case with VG`s on the underside of the tailplane and the
elevator in
the `up` position they would do exactly what they do on the top of
a wing.
Keep the boundary layer from breaking away. That would increase the
effectiveness of the `up` elevator.

Can you prove or disprove?

Cheers

Pat

do not archive

--





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Thom Riddle



Joined: 10 Jan 2006
Posts: 1597
Location: Buffalo, NY, USA (9G0)

PostPosted: Wed Mar 29, 2006 6:16 am    Post subject: Land Shorter VG's on Firestar II Reply with quote

Possums,

My comment about JOA's lost credibility had to do with his statement
that the VGs on the tail would enable the standard gear leg Kolb to
land at high angles of attack without the tail hitting first. This
could only be true if the tail was generating UPWARDS lift which is
most definitely not the case in a Kolb with the stick back and nose
pitching upwards. By definition, a high wing AOA the tail is low, so
JOAs statement is clearly impossible.

My comment had nothing to do with the location of the VGs on the tail.
I agree that with the normal configuration horizontal stabilizer (the
tail lift vector is down) the VGs on the bottom could help generate
more downward lift at high TAIL AOA. High tail AOA (stick all the way
back) produces low tail position relative to the rest of the airplane.

I hope this clears up my statement, probably didn't but that is the
best I can do.

Thom in Buffalo
do not archive


At 07:40 AM 3/27/2006, you wrote:
>
<jtriddle(at)adelphia.net>
>
>This JOA guy has lost all credibility with me due to his
statement
>about the tail stalling first causing the tail to be low.
I don't know about that - if you do a Google Search on
"horizontal stabilizer" & "vortex generators" you will find out
that everybody recommends putting them on the "bottom" of
the Horizontal stabilizer, not just this JOA guy. Even in the
GA planes.


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Possum



Joined: 12 Jan 2006
Posts: 112
Location: Georgia

PostPosted: Sat Apr 01, 2006 8:12 pm    Post subject: Land Shorter VG's on Firestar II Reply with quote

At 09:54 AM 3/28/2006, you wrote:
Quote:


Group,

Joa did respond to the list last night. I should read everything
before I reply to anything in the morning. He changed the subject line.

Anyway, what he accomplished with VGs on the underside of the
horizontal stab is exactly the way my Firestar II flys now. So
adding them to my stab would be a waste of time and money.

--------
John Jung

John
I'll agree with you on that .... but since I ordered another 20 VGs,
I thought I would put them on either side of the Rudder.
So, today I spent 45 minutes with my nose stuck up in the air...at
"what ever angle" it is at 29 - 32 mph and
testing the rudder input. You may not have noticed yet that when you
slow the stall speed down that much with
the VGs, the rudder does not respond like it did at 40 mph. Well, I
think you will recover the difference by
installing those little things ...like he says - in front of the
rudder hinges. Flying 30+- mph indicated - thermals, not too
bad ( but bad enough that no one else was flying ), still drops a
wing once in a while, kick the opposite rudder, and it picks it right
back up again. Used to be sloppy. I've got cars stopping below me -
thinking I'm some kind of a box-kite ...cool. Another $ 30 well spent !!


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planecrazzzy
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PostPosted: Sun Apr 02, 2006 1:25 pm    Post subject: Re: Land Shorter VG's on Firestar II Reply with quote

Hey Possum,
Can you post some more pictures ???
.
.
Thanks,
.
. Gotta Fly...
Mike in MN / N381PM
.
.
.
.

[/quote]
John
I'll agree with you on that .... but since I ordered another 20 VGs,
I thought I would put them on either side of the Rudder.
So, today I spent 45 minutes with my nose stuck up in the air...at
"what ever angle" it is at 29 - 32 mph and
testing the rudder input. You may not have noticed yet that when you
slow the stall speed down that much with
the VGs, the rudder does not respond like it did at 40 mph. Well, I
think you will recover the difference by
installing those little things ...like he says - in front of the
rudder hinges. Flying 30+- mph indicated - thermals, not too
bad ( but bad enough that no one else was flying ), still drops a
wing once in a while, kick the opposite rudder, and it picks it right
back up again. Used to be sloppy. I've got cars stopping below me -
thinking I'm some kind of a box-kite ...cool. Another $ 30 well spent !![/quote]


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