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[rebel-builders] VG location--from a VG manufacturer

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WALTER KLATT

[rebel-builders] VG location--from a VG manufacturer

Post by WALTER KLATT » Sun Feb 19, 2012 5:37 pm

Yeah, there are quite a few VG makers now, but they all say pretty well the same thing as to effectiveness and placement. There might be slight variations in how they measure the position, and good to see competition live and well, with their claims.

I have the "plastic shark fin" type (landshorter.com), and they seem to work fine for me. They have their own claims as to why they are better. But the only thing I can confirm, is that they are cheaper than the others.

Dennis here, has the PNW ones on his Elite (same placement as mine), and they seem to work very well for him, too.

Can't remember who, but I thought someone mentioned on the list said that they didn't do anything for elevator authority. However, I thought someone else tried them there and they did help, so not sure about that. I was thinking of trying it on my Rebel, just to see if there is any difference. Having said that, I don't have any problem with the Rebel on floats as to elevator and hor stab effectiveness. I think the extra speed (airflow) for landing on floats is enough to keep the elevator effective. But then again, I may not know what I am missing.

Walter

----- Original Message -----
From: Ted Waltman <ted@vafm.org>
Date: Tuesday, October 13, 2009 9:42 am
Subject: [rebel-builders] VG location--from a VG manufacturer
To: rebel-builders@dcsol.com
See the vendor comments below regarding the discussion on the
builder's list
regarding VG location. Al Paxhia and I both have their
VG's on our Moose.



Link to their website: http://www.pnwaero.com/



Ted Waltman



From: PNWAero [mailto:aero@pnwaero.com]
Sent: Friday, October 09, 2009 9:34 AM
To: Ted Waltman
Subject: RE: VG location--existing customer



Hi Ted:



In regards to your question: I generally start at 10% of the
chord and have
never placed them further back than 11% because of loss of
effectiveness. I
very rarely go past 9% because of the potential for loss of top
speed of the
aircraft. All measurements are to the leading edge of the VG not
to the
center of the VG. The chord is measured with the flaps up.



This information is based on our blade style VGs that we
manufacture which
includes the same shape that the certified aircraft use. It's
our experience
over the years that the delta shape (or shark fin) type of VG is less
effective and may require a different location.



Hope things are going well for you.



Best regards,

Jerry
Pacific Northwest Aero LLC

-----Original Message-----
From: Ted Waltman [mailto:tedwaltman@gmail.com]
Sent: Thursday, October 08, 2009 7:55 AM
To: aero@pnwaero.com
Subject: VG location--existing customer

Hello folks!



I've had your VG's on my Moose for several years. Great
product, as my
testimonial on your website indicates.



There's a debate going on within the Moose builders email list
regarding VG
location. One figure being discussed indicates that the
center of the VG
should be at the 10% chord location.



I have two questions:



- Do you
have any general recommendation based on customer or your
own experience regarding % chord location for VG's?



- Is %
chord established by measuring from the front of the wing to
the trailing edge of the flaps-with the flaps up or down (I
assume down)?





Thank you,



Ted Waltman

Murphy Moose





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kyle martin

[rebel-builders] VG location--from a VG manufacturer

Post by kyle martin » Sun Feb 19, 2012 5:37 pm

Take a look at boundary layer research's (BLR) design for the PA-18
SuperCub, now owned by Cub Crafters, where they put a 'strake', which is
basically a deflector fin, forward and below the horizontal stab so as to
force air under the stab and elev and increase their effectiveness, and
reduce tendency to stall, especially at slow airspeeds, and extreme
attitudes. you can find photos online of the placement and design. supercub
owners are very happy with the design, and there have been far fewer tail
stall crashes since. tail surfaces aren't all airfoils in all cases, so VG's
wont always do a lot. cheers

On Tue, Oct 13, 2009 at 2:41 PM, WALTER KLATT <Walter.Klatt@shaw.ca> wrote:
Yeah, there are quite a few VG makers now, but they all say pretty well the
same thing as to effectiveness and placement. There might be slight
variations in how they measure the position, and good to see competition
live and well, with their claims.

I have the "plastic shark fin" type (landshorter.com), and they seem to
work fine for me. They have their own claims as to why they are better. But
the only thing I can confirm, is that they are cheaper than the others.

Dennis here, has the PNW ones on his Elite (same placement as mine), and
they seem to work very well for him, too.

Can't remember who, but I thought someone mentioned on the list said that
they didn't do anything for elevator authority. However, I thought someone
else tried them there and they did help, so not sure about that. I was
thinking of trying it on my Rebel, just to see if there is any difference.
Having said that, I don't have any problem with the Rebel on floats as to
elevator and hor stab effectiveness. I think the extra speed (airflow) for
landing on floats is enough to keep the elevator effective. But then again,
I may not know what I am missing.

Walter

----- Original Message -----
From: Ted Waltman <ted@vafm.org>
Date: Tuesday, October 13, 2009 9:42 am
Subject: [rebel-builders] VG location--from a VG manufacturer
To: rebel-builders@dcsol.com
See the vendor comments below regarding the discussion on the
builder's list
regarding VG location. Al Paxhia and I both have their
VG's on our Moose.



Link to their website: http://www.pnwaero.com/



Ted Waltman



From: PNWAero [mailto:aero@pnwaero.com]
Sent: Friday, October 09, 2009 9:34 AM
To: Ted Waltman
Subject: RE: VG location--existing customer



Hi Ted:



In regards to your question: I generally start at 10% of the
chord and have
never placed them further back than 11% because of loss of
effectiveness. I
very rarely go past 9% because of the potential for loss of top
speed of the
aircraft. All measurements are to the leading edge of the VG not
to the
center of the VG. The chord is measured with the flaps up.



This information is based on our blade style VGs that we
manufacture which
includes the same shape that the certified aircraft use. It's
our experience
over the years that the delta shape (or shark fin) type of VG is less
effective and may require a different location.



Hope things are going well for you.



Best regards,

Jerry
Pacific Northwest Aero LLC

-----Original Message-----
From: Ted Waltman [mailto:tedwaltman@gmail.com]
Sent: Thursday, October 08, 2009 7:55 AM
To: aero@pnwaero.com
Subject: VG location--existing customer

Hello folks!



I've had your VG's on my Moose for several years. Great
product, as my
testimonial on your website indicates.



There's a debate going on within the Moose builders email list
regarding VG
location. One figure being discussed indicates that the
center of the VG
should be at the 10% chord location.



I have two questions:



- Do you
have any general recommendation based on customer or your
own experience regarding % chord location for VG's?



- Is %
chord established by measuring from the front of the wing to
the trailing edge of the flaps-with the flaps up or down (I
assume down)?





Thank you,



Ted Waltman

Murphy Moose





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WALTER KLATT

[rebel-builders] VG location--from a VG manufacturer

Post by WALTER KLATT » Sun Feb 19, 2012 5:37 pm

Do you have a link for that?

----- Original Message -----
From: kyle martin <alpsnowman@gmail.com>
Date: Tuesday, October 13, 2009 2:56 pm
Subject: Re: [rebel-builders] VG location--from a VG manufacturer
To: rebel-builders@dcsol.com
Take a look at boundary layer research's (BLR) design for the PA-18
SuperCub, now owned by Cub Crafters, where they put a 'strake',
which is
basically a deflector fin, forward and below the horizontal stab
so as to
force air under the stab and elev and increase their
effectiveness, and
reduce tendency to stall, especially at slow airspeeds, and extreme
attitudes. you can find photos online of the placement and
design. supercub
owners are very happy with the design, and there have been far
fewer tail
stall crashes since. tail surfaces aren't all airfoils in all
cases, so VG's
wont always do a lot. cheers

On Tue, Oct 13, 2009 at 2:41 PM, WALTER KLATT
<Walter.Klatt@shaw.ca> wrote:
Yeah, there are quite a few VG makers now, but they all say
pretty well the
same thing as to effectiveness and placement. There might be slight
variations in how they measure the position, and good to see
competition> live and well, with their claims.
I have the "plastic shark fin" type (landshorter.com),
and they seem to
work fine for me. They have their own claims as to why they
are better. But
the only thing I can confirm, is that they are cheaper than
the others.
Dennis here, has the PNW ones on his Elite (same placement as
mine), and
they seem to work very well for him, too.

Can't remember who, but I thought someone mentioned on the
list said that
they didn't do anything for elevator authority. However, I
thought someone
else tried them there and they did help, so not sure about
that. I was
thinking of trying it on my Rebel, just to see if there is any
difference.> Having said that, I don't have any problem with the
Rebel on floats as to
elevator and hor stab effectiveness. I think the extra speed
(airflow) for
landing on floats is enough to keep the elevator effective.
But then again,
I may not know what I am missing.

Walter

----- Original Message -----
From: Ted Waltman <ted@vafm.org>
Date: Tuesday, October 13, 2009 9:42 am
Subject: [rebel-builders] VG location--from a VG manufacturer
To: rebel-builders@dcsol.com
See the vendor comments below regarding the discussion on the
builder's list
regarding VG location. Al Paxhia and I both have their
VG's on our Moose.



Link to their website: http://www.pnwaero.com/



Ted Waltman



From: PNWAero [mailto:aero@pnwaero.com]
Sent: Friday, October 09, 2009 9:34 AM
To: Ted Waltman
Subject: RE: VG location--existing customer



Hi Ted:



In regards to your question: I generally start at 10% of the
chord and have
never placed them further back than 11% because of loss of
effectiveness. I
very rarely go past 9% because of the potential for loss of top
speed of the
aircraft. All measurements are to the leading edge of the VG not
to the
center of the VG. The chord is measured with the flaps up.



This information is based on our blade style VGs that we
manufacture which
includes the same shape that the certified aircraft use. It's
our experience
over the years that the delta shape (or shark fin) type of
VG is less
effective and may require a different location.



Hope things are going well for you.



Best regards,

Jerry
Pacific Northwest Aero LLC

-----Original Message-----
From: Ted Waltman [mailto:tedwaltman@gmail.com]
Sent: Thursday, October 08, 2009 7:55 AM
To: aero@pnwaero.com
Subject: VG location--existing customer

Hello folks!



I've had your VG's on my Moose for several years. Great
product, as my
testimonial on your website indicates.



There's a debate going on within the Moose builders email list
regarding VG
location. One figure being discussed indicates that the
center of the VG
should be at the 10% chord location.



I have two questions:



- Do you
have any general recommendation based on customer or your
own experience regarding % chord location for VG's?



- Is %
chord established by measuring from the front of the wing to
the trailing edge of the flaps-with the flaps up or down (I
assume down)?





Thank you,



Ted Waltman

Murphy Moose





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kyle martin

[rebel-builders] VG location--from a VG manufacturer

Post by kyle martin » Sun Feb 19, 2012 5:37 pm

http://www.cubcrafters.com/services/par ... ors_02.jpg

http://www.cubcrafters.com/services/par ... ors_01.jpg

you will have to just browse thru photos of super cubs (pa-18) to try and
get a more detailed photo of what exactly it looks like and its placement
(strake).

On Tue, Oct 13, 2009 at 3:13 PM, WALTER KLATT <Walter.Klatt@shaw.ca> wrote:
Do you have a link for that?

----- Original Message -----
From: kyle martin <alpsnowman@gmail.com>
Date: Tuesday, October 13, 2009 2:56 pm
Subject: Re: [rebel-builders] VG location--from a VG manufacturer
To: rebel-builders@dcsol.com
Take a look at boundary layer research's (BLR) design for the PA-18
SuperCub, now owned by Cub Crafters, where they put a 'strake',
which is
basically a deflector fin, forward and below the horizontal stab
so as to
force air under the stab and elev and increase their
effectiveness, and
reduce tendency to stall, especially at slow airspeeds, and extreme
attitudes. you can find photos online of the placement and
design. supercub
owners are very happy with the design, and there have been far
fewer tail
stall crashes since. tail surfaces aren't all airfoils in all
cases, so VG's
wont always do a lot. cheers

On Tue, Oct 13, 2009 at 2:41 PM, WALTER KLATT
<Walter.Klatt@shaw.ca> wrote:
Yeah, there are quite a few VG makers now, but they all say
pretty well the
same thing as to effectiveness and placement. There might be slight
variations in how they measure the position, and good to see
competition> live and well, with their claims.
I have the "plastic shark fin" type (landshorter.com),
and they seem to
work fine for me. They have their own claims as to why they
are better. But
the only thing I can confirm, is that they are cheaper than
the others.
Dennis here, has the PNW ones on his Elite (same placement as
mine), and
they seem to work very well for him, too.

Can't remember who, but I thought someone mentioned on the
list said that
they didn't do anything for elevator authority. However, I
thought someone
else tried them there and they did help, so not sure about
that. I was
thinking of trying it on my Rebel, just to see if there is any
difference.> Having said that, I don't have any problem with the
Rebel on floats as to
elevator and hor stab effectiveness. I think the extra speed
(airflow) for
landing on floats is enough to keep the elevator effective.
But then again,
I may not know what I am missing.

Walter

----- Original Message -----
From: Ted Waltman <ted@vafm.org>
Date: Tuesday, October 13, 2009 9:42 am
Subject: [rebel-builders] VG location--from a VG manufacturer
To: rebel-builders@dcsol.com
VG is less
----
----



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WALTER KLATT

[rebel-builders] VG location--from a VG manufacturer

Post by WALTER KLATT » Sun Feb 19, 2012 5:37 pm

Hmmm, interesting... Especially those strakes. I have another airplane (not the Rebel) that has a definite elevator effectiveness problem under certain conditions. That's why I bought the VGs in the first place. I tried them under the hor stab, but they didn't help one bit there. And on the wings, they helped only slightly.

Then I tried them on the Rebel with 2 sided tape, since I had them anyway, and was very pleasantly surprised by the results.

But maybe these strakes could help with this other airplane... Off topic for this list, but thanks for the info.

Walter

----- Original Message -----
From: kyle martin <alpsnowman@gmail.com>
Date: Tuesday, October 13, 2009 3:29 pm
Subject: Re: [rebel-builders] VG location--from a VG manufacturer
To: rebel-builders@dcsol.com
http://www.cubcrafters.com/services/par ... cm_vortex-
generators_02.jpg
http://www.cubcrafters.com/services/par ... cm_vortex-
generators_01.jpg
you will have to just browse thru photos of super cubs (pa-18)
to try and
get a more detailed photo of what exactly it looks like and its
placement(strake).

On Tue, Oct 13, 2009 at 3:13 PM, WALTER KLATT
<Walter.Klatt@shaw.ca> wrote:
Do you have a link for that?

----- Original Message -----
From: kyle martin <alpsnowman@gmail.com>
Date: Tuesday, October 13, 2009 2:56 pm
Subject: Re: [rebel-builders] VG location--from a VG manufacturer
To: rebel-builders@dcsol.com
Take a look at boundary layer research's (BLR) design for
the PA-18
SuperCub, now owned by Cub Crafters, where they put a 'strake',
which is
basically a deflector fin, forward and below the horizontal stab
so as to
force air under the stab and elev and increase their
effectiveness, and
reduce tendency to stall, especially at slow airspeeds, and
extreme> > attitudes. you can find photos online of the
placement and
design. supercub
owners are very happy with the design, and there have been far
fewer tail
stall crashes since. tail surfaces aren't all airfoils in all
cases, so VG's
wont always do a lot. cheers

On Tue, Oct 13, 2009 at 2:41 PM, WALTER KLATT
<Walter.Klatt@shaw.ca> wrote:
pretty well the
be slight
competition> live and well, with their claims. and they seem to are better. But the others. mine), and list said that thought someone that. I was difference.> Having said that, I don't have any problem with the
Rebel on floats as to (airflow) for But then again,
on the
of top
the VG not
VG is less
email list
that the
Do you
Is %
wing to
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Ron Shannon

[rebel-builders] VG location--from a VG manufacturer

Post by Ron Shannon » Sun Feb 19, 2012 5:37 pm

Thanks for that info, Kyle. It would be interesting to learn if / when
anyone has experience with the two placement zones on the Rebel, e.g., a
section on the outer wing where the VG's are set further forward, no doubt
to delay stall of the outer wing. Perhaps with the Rebel's full flaperons,
it wouldn't make as much sense.

Ron
254R


On Tue, Oct 13, 2009 at 3:27 PM, kyle martin <alpsnowman@gmail.com> wrote:
http://www.cubcrafters.com/services/par ... ors_02.jpg


http://www.cubcrafters.com/services/par ... ors_01.jpg

you will have to just browse thru photos of super cubs (pa-18) to try and
get a more detailed photo of what exactly it looks like and its placement
(strake).



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Bob Patterson

[rebel-builders] VG location--from a VG manufacturer

Post by Bob Patterson » Sun Feb 19, 2012 5:37 pm

Hi Walter !

The main reason for the strakes on the Smith Cub was an
extreme forward C of G position, amplified by the increased
wing span & flap size, which decreased the effectiveness of
the stab. Strakes have long been used to increase the effectiveness
of the stab - the British Tiger Moths needed strakes for spin recovery,
maybe because they had automatic slats on the wings. Canadian
Tigers did not have strakes ....

I've wondered if Elites might benefit from strakes ...

--
......bobp
bobp@prosumers.ca

http://bpatterson.qhealthbeauty.com
http://apatterson2.ordermygift.com

Any views expressed in this message are those of the individual sender
and do not necessarily reflect the views of any other entities or persons.
Any action taken as a result of the contents of this email is totally the
responsibility of the reader.

-------------------------------orig.-------------------------
On Tuesday 13 October 2009 22:59, WALTER KLATT wrote:
Hmmm, interesting... Especially those strakes. I have another airplane
(not the Rebel) that has a definite elevator effectiveness problem under
certain conditions. That's why I bought the VGs in the first place. I
tried them under the hor stab, but they didn't help one bit there. And on
the wings, they helped only slightly.

Then I tried them on the Rebel with 2 sided tape, since I had them anyway,
and was very pleasantly surprised by the results.

But maybe these strakes could help with this other airplane... Off topic
for this list, but thanks for the info.

Walter

----- Original Message -----
From: kyle martin <alpsnowman@gmail.com>
Date: Tuesday, October 13, 2009 3:29 pm
Subject: Re: [rebel-builders] VG location--from a VG manufacturer
To: rebel-builders@dcsol.com
http://www.cubcrafters.com/services/par ... cm_vortex-
generators_02.jpg
http://www.cubcrafters.com/services/par ... cm_vortex-
generators_01.jpg
you will have to just browse thru photos of super cubs (pa-18)
to try and
get a more detailed photo of what exactly it looks like and its
placement(strake).

On Tue, Oct 13, 2009 at 3:13 PM, WALTER KLATT

<Walter.Klatt@shaw.ca> wrote:
Do you have a link for that?

----- Original Message -----
From: kyle martin <alpsnowman@gmail.com>
Date: Tuesday, October 13, 2009 2:56 pm
Subject: Re: [rebel-builders] VG location--from a VG manufacturer
To: rebel-builders@dcsol.com
the PA-18
extreme> > attitudes. you can find photos online of the
placement and
be slight
on the
of top
the VG not
email list
that the
Do you
Is %
wing to


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Walter Klatt

[rebel-builders] VG location--from a VG manufacturer

Post by Walter Klatt » Sun Feb 19, 2012 5:40 pm

Nah, the Elites need more than that... Like maybe a smaller tail, lighter
ailerons/flaps, lighter fuselage, lighter... Ah, but then it would be a
Rebel... LOL

Walter (ducking and running)

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On Behalf Of Bob
Patterson
Sent: October 13, 2009 4:40 PM
To: rebel-builders@dcsol.com
Subject: Re: [rebel-builders] VG location--from a VG manufacturer


Hi Walter !

The main reason for the strakes on the Smith Cub was an
extreme forward C of G position, amplified by the increased
wing span & flap size, which decreased the effectiveness of
the stab. Strakes have long been used to increase the effectiveness
of the stab - the British Tiger Moths needed strakes for spin recovery,
maybe because they had automatic slats on the wings. Canadian
Tigers did not have strakes ....

I've wondered if Elites might benefit from strakes ...

--
......bobp
bobp@prosumers.ca

http://bpatterson.qhealthbeauty.com
http://apatterson2.ordermygift.com

Any views expressed in this message are those of the individual sender
and do not necessarily reflect the views of any other entities or persons.
Any action taken as a result of the contents of this email is totally the
responsibility of the reader.

-------------------------------orig.-------------------------
On Tuesday 13 October 2009 22:59, WALTER KLATT wrote:
Hmmm, interesting... Especially those strakes. I have another airplane
(not the Rebel) that has a definite elevator effectiveness problem under
certain conditions. That's why I bought the VGs in the first place. I
tried them under the hor stab, but they didn't help one bit there. And on
the wings, they helped only slightly.

Then I tried them on the Rebel with 2 sided tape, since I had them anyway,
and was very pleasantly surprised by the results.

But maybe these strakes could help with this other airplane... Off topic
for this list, but thanks for the info.

Walter

----- Original Message -----
From: kyle martin <alpsnowman@gmail.com>
Date: Tuesday, October 13, 2009 3:29 pm
Subject: Re: [rebel-builders] VG location--from a VG manufacturer
To: rebel-builders@dcsol.com
http://www.cubcrafters.com/services/par ... cm_vortex-
generators_02.jpg
http://www.cubcrafters.com/services/par ... cm_vortex-
generators_01.jpg
you will have to just browse thru photos of super cubs (pa-18)
to try and
get a more detailed photo of what exactly it looks like and its
placement(strake).

On Tue, Oct 13, 2009 at 3:13 PM, WALTER KLATT

<Walter.Klatt@shaw.ca> wrote:
Do you have a link for that?

----- Original Message -----
From: kyle martin <alpsnowman@gmail.com>
Date: Tuesday, October 13, 2009 2:56 pm
Subject: Re: [rebel-builders] VG location--from a VG manufacturer
To: rebel-builders@dcsol.com
the PA-18
extreme> > attitudes. you can find photos online of the
placement and
be slight
on the
of top
the VG not
email list
that the
Do you
Is %
wing to


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Bob Andrews

[rebel-builders] VG location--from a VG manufacturer

Post by Bob Andrews » Sun Feb 19, 2012 5:40 pm

Yeh ... ducking ... running ... and feet don't fail me now !! LOL

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On Behalf Of Walter
Klatt
Sent: Tuesday, October 13, 2009 4:58 PM
To: rebel-builders@dcsol.com
Subject: RE: [rebel-builders] VG location--from a VG manufacturer

Nah, the Elites need more than that... Like maybe a smaller tail, lighter
ailerons/flaps, lighter fuselage, lighter... Ah, but then it would be a
Rebel... LOL

Walter (ducking and running)

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On Behalf Of Bob
Patterson
Sent: October 13, 2009 4:40 PM
To: rebel-builders@dcsol.com
Subject: Re: [rebel-builders] VG location--from a VG manufacturer


Hi Walter !

The main reason for the strakes on the Smith Cub was an
extreme forward C of G position, amplified by the increased
wing span & flap size, which decreased the effectiveness of
the stab. Strakes have long been used to increase the effectiveness
of the stab - the British Tiger Moths needed strakes for spin recovery,
maybe because they had automatic slats on the wings. Canadian
Tigers did not have strakes ....

I've wondered if Elites might benefit from strakes ...

--
......bobp
bobp@prosumers.ca

http://bpatterson.qhealthbeauty.com
http://apatterson2.ordermygift.com

Any views expressed in this message are those of the individual sender
and do not necessarily reflect the views of any other entities or persons.
Any action taken as a result of the contents of this email is totally the
responsibility of the reader.

-------------------------------orig.-------------------------
On Tuesday 13 October 2009 22:59, WALTER KLATT wrote:
Hmmm, interesting... Especially those strakes. I have another airplane
(not the Rebel) that has a definite elevator effectiveness problem under
certain conditions. That's why I bought the VGs in the first place. I
tried them under the hor stab, but they didn't help one bit there. And on
the wings, they helped only slightly.

Then I tried them on the Rebel with 2 sided tape, since I had them anyway,
and was very pleasantly surprised by the results.

But maybe these strakes could help with this other airplane... Off topic
for this list, but thanks for the info.

Walter

----- Original Message -----
From: kyle martin <alpsnowman@gmail.com>
Date: Tuesday, October 13, 2009 3:29 pm
Subject: Re: [rebel-builders] VG location--from a VG manufacturer
To: rebel-builders@dcsol.com
http://www.cubcrafters.com/services/par ... cm_vortex-
generators_02.jpg
http://www.cubcrafters.com/services/par ... cm_vortex-
generators_01.jpg
you will have to just browse thru photos of super cubs (pa-18)
to try and
get a more detailed photo of what exactly it looks like and its
placement(strake).

On Tue, Oct 13, 2009 at 3:13 PM, WALTER KLATT

<Walter.Klatt@shaw.ca> wrote:
Do you have a link for that?

----- Original Message -----
From: kyle martin <alpsnowman@gmail.com>
Date: Tuesday, October 13, 2009 2:56 pm
Subject: Re: [rebel-builders] VG location--from a VG manufacturer
To: rebel-builders@dcsol.com
the PA-18
extreme> > attitudes. you can find photos online of the
placement and
be slight
on the
of top
the VG not
email list
that the
Do you
Is %
wing to


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