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[rebel-builders] Measuring chord for VG's

Converted from Wildcat! database. (read only)
Bob Patterson

[rebel-builders] Measuring chord for VG's

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

Hi Ted !

It's always flaps up - should be the same as the Rebel = 60 inches.

--
......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 Thursday 08 October 2009 14:35, Ted Waltman wrote:
Are folks measuring chord from wing front to flap-end with the flaps up or
down?



Anyone know what the chord is of a Super Rebel or Moose (with flaps up &
flaps down)?



Thanks!



Ted



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Ted Waltman

[rebel-builders] Measuring chord for VG's

Post by Ted Waltman » Sun Feb 19, 2012 5:37 pm

Not being an aerodynamic engineer, why is it always flaps-up? Wouldn't you
want to optimize VG performance in the typical landing configuration, e.g.
flaps down? Any information much appreciated.

Ted

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On Behalf Of Bob
Patterson
Sent: Thursday, October 08, 2009 8:55 AM
To: rebel-builders@dcsol.com
Subject: Re: [rebel-builders] Measuring chord for VG's


Hi Ted !

It's always flaps up - should be the same as the Rebel = 60 inches.

--
......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 Thursday 08 October 2009 14:35, Ted Waltman wrote:
Are folks measuring chord from wing front to flap-end with the flaps up or
down?



Anyone know what the chord is of a Super Rebel or Moose (with flaps up &
flaps down)?



Thanks!



Ted



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WALTER KLATT

[rebel-builders] Measuring chord for VG's

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

Ted, I think it is just the way the VG manufacturers do their their testing and how they define their placement. If you talk to them, I am sure they will say measure with your flaps in neutral.

They will have different placement recommendations for different types of planes. 10% is what seems to work best for our wings. I have another plane with them, and they have to be at the 6 % location to get maximum benefit. And even then it turned out to only lower stall by about 2 mph, although it did firm up the ailerons at low speed. The Rebel, on the other hand, lowered stall by 8 - 10 mph, which is a lot. Also think it improved climb rate (from my earlier testing with the 320), but that is very hard to prove. You sure notice the VGs on water take-offs, though.

Walter

----- Original Message -----
From: Ted Waltman <ted@vafm.org>
Date: Thursday, October 8, 2009 8:01 am
Subject: RE: [rebel-builders] Measuring chord for VG's
To: rebel-builders@dcsol.com
Not being an aerodynamic engineer, why is it always flaps-
up? Wouldn't you
want to optimize VG performance in the typical landing
configuration, e.g.
flaps down? Any information much appreciated.

Ted

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On
Behalf Of Bob
Patterson
Sent: Thursday, October 08, 2009 8:55 AM
To: rebel-builders@dcsol.com
Subject: Re: [rebel-builders] Measuring chord for VG's


Hi Ted !

It's always flaps up - should be the
same as the Rebel = 60 inches.

--
......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 Thursday 08 October 2009 14:35, Ted Waltman wrote:
Are folks measuring chord from wing front to flap-end with the
flaps up or
down?



Anyone know what the chord is of a Super Rebel or Moose (with
flaps up &
flaps down)?



Thanks!



Ted



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David Jackson

[rebel-builders] Measuring chord for VG's

Post by David Jackson » Sun Feb 19, 2012 5:37 pm

Don't forget what the Vortex generators do - generate vortexs. In order to do that they have to be outside of the boundary layer airflow to generate a vortex to break up the boundary layer and move the flow separation point further back. Moving them further back on a wing just because it has a longer chord could move them to an area where they are inside the boundary layer and cannot generate vortexs because there is not enough airflow over them.



I believe Walter is correct when he says 10% is a start point that the VG manufacturers use to test. Since we are the manufacturers for our aircraft we could experiment with different positions to see what works best. I have read that double-sided tape will hold the VGs in position well enough for testing purposes but am personally a long way away from doing that.



Dave J
Date: Thu, 8 Oct 2009 08:16:27 -0700
From: Walter.Klatt@shaw.ca
Subject: Re: RE: [rebel-builders] Measuring chord for VG's
To: rebel-builders@dcsol.com

Ted, I think it is just the way the VG manufacturers do their their testing and how they define their placement. If you talk to them, I am sure they will say measure with your flaps in neutral.

They will have different placement recommendations for different types of planes. 10% is what seems to work best for our wings. I have another plane with them, and they have to be at the 6 % location to get maximum benefit. And even then it turned out to only lower stall by about 2 mph, although it did firm up the ailerons at low speed. The Rebel, on the other hand, lowered stall by 8 - 10 mph, which is a lot. Also think it improved climb rate (from my earlier testing with the 320), but that is very hard to prove. You sure notice the VGs on water take-offs, though.

Walter

----- Original Message -----
From: Ted Waltman <ted@vafm.org>
Date: Thursday, October 8, 2009 8:01 am
Subject: RE: [rebel-builders] Measuring chord for VG's
To: rebel-builders@dcsol.com
Not being an aerodynamic engineer, why is it always flaps-
up? Wouldn't you
want to optimize VG performance in the typical landing
configuration, e.g.
flaps down? Any information much appreciated.

Ted

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On
Behalf Of Bob
Patterson
Sent: Thursday, October 08, 2009 8:55 AM
To: rebel-builders@dcsol.com
Subject: Re: [rebel-builders] Measuring chord for VG's


Hi Ted !

It's always flaps up - should be the
same as the Rebel = 60 inches.

--
......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 Thursday 08 October 2009 14:35, Ted Waltman wrote:
Are folks measuring chord from wing front to flap-end with the
flaps up or
down?



Anyone know what the chord is of a Super Rebel or Moose (with
flaps up &
flaps down)?



Thanks!



Ted



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Jones, Michael

[rebel-builders] Measuring chord for VG's

Post by Jones, Michael » Sun Feb 19, 2012 5:37 pm

Has any one put vortex generators on the horizontal or verticla tail
plans ???

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On Behalf Of
David Jackson
Sent: October 8, 2009 2:03 PM
To: Rebel Builders
Subject: RE: [rebel-builders] Measuring chord for VG's

Don't forget what the Vortex generators do - generate vortexs. In order
to do that they have to be outside of the boundary layer airflow to
generate a vortex to break up the boundary layer and move the flow
separation point further back. Moving them further back on a wing just
because it has a longer chord could move them to an area where they are
inside the boundary layer and cannot generate vortexs because there is
not enough airflow over them.



I believe Walter is correct when he says 10% is a start point that the
VG manufacturers use to test. Since we are the manufacturers for our
aircraft we could experiment with different positions to see what works
best. I have read that double-sided tape will hold the VGs in position
well enough for testing purposes but am personally a long way away from
doing that.



Dave J
Date: Thu, 8 Oct 2009 08:16:27 -0700
From: Walter.Klatt@shaw.ca
Subject: Re: RE: [rebel-builders] Measuring chord for VG's
To: rebel-builders@dcsol.com

Ted, I think it is just the way the VG manufacturers do their their
testing and how they define their placement. If you talk to them, I am
sure they will say measure with your flaps in neutral.
They will have different placement recommendations for different types
of planes. 10% is what seems to work best for our wings. I have another
plane with them, and they have to be at the 6 % location to get maximum
benefit. And even then it turned out to only lower stall by about 2 mph,
although it did firm up the ailerons at low speed. The Rebel, on the
other hand, lowered stall by 8 - 10 mph, which is a lot. Also think it
improved climb rate (from my earlier testing with the 320), but that is
very hard to prove. You sure notice the VGs on water take-offs, though.
Walter

----- Original Message -----
From: Ted Waltman <ted@vafm.org>
Date: Thursday, October 8, 2009 8:01 am
Subject: RE: [rebel-builders] Measuring chord for VG's
To: rebel-builders@dcsol.com
Not being an aerodynamic engineer, why is it always flaps-
up? Wouldn't you
want to optimize VG performance in the typical landing
configuration, e.g.
flaps down? Any information much appreciated.

Ted

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On
Behalf Of Bob
Patterson
Sent: Thursday, October 08, 2009 8:55 AM
To: rebel-builders@dcsol.com
Subject: Re: [rebel-builders] Measuring chord for VG's


Hi Ted !

It's always flaps up - should be the
same as the Rebel = 60 inches.

--
......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 Thursday 08 October 2009 14:35, Ted Waltman wrote:
Are folks measuring chord from wing front to flap-end with the
flaps up or
down?



Anyone know what the chord is of a Super Rebel or Moose (with
flaps up &
flaps down)?



Thanks!



Ted



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Ted Waltman

[rebel-builders] Measuring chord for VG's

Post by Ted Waltman » Sun Feb 19, 2012 5:37 pm

Yes, I put them on the h-stab (bottom of course) and the vertical fin. I
suspect the vertical fin install is more useful (designed for?) float
operations?

Ted

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On Behalf Of Jones,
Michael
Sent: Thursday, October 08, 2009 12:47 PM
To: rebel-builders@dcsol.com
Subject: RE: [rebel-builders] Measuring chord for VG's

Has any one put vortex generators on the horizontal or verticla tail
plans ???

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On Behalf Of
David Jackson
Sent: October 8, 2009 2:03 PM
To: Rebel Builders
Subject: RE: [rebel-builders] Measuring chord for VG's

Don't forget what the Vortex generators do - generate vortexs. In order
to do that they have to be outside of the boundary layer airflow to
generate a vortex to break up the boundary layer and move the flow
separation point further back. Moving them further back on a wing just
because it has a longer chord could move them to an area where they are
inside the boundary layer and cannot generate vortexs because there is
not enough airflow over them.



I believe Walter is correct when he says 10% is a start point that the
VG manufacturers use to test. Since we are the manufacturers for our
aircraft we could experiment with different positions to see what works
best. I have read that double-sided tape will hold the VGs in position
well enough for testing purposes but am personally a long way away from
doing that.



Dave J
Date: Thu, 8 Oct 2009 08:16:27 -0700
From: Walter.Klatt@shaw.ca
Subject: Re: RE: [rebel-builders] Measuring chord for VG's
To: rebel-builders@dcsol.com

Ted, I think it is just the way the VG manufacturers do their their
testing and how they define their placement. If you talk to them, I am
sure they will say measure with your flaps in neutral.
They will have different placement recommendations for different types
of planes. 10% is what seems to work best for our wings. I have another
plane with them, and they have to be at the 6 % location to get maximum
benefit. And even then it turned out to only lower stall by about 2 mph,
although it did firm up the ailerons at low speed. The Rebel, on the
other hand, lowered stall by 8 - 10 mph, which is a lot. Also think it
improved climb rate (from my earlier testing with the 320), but that is
very hard to prove. You sure notice the VGs on water take-offs, though.
Walter

----- Original Message -----
From: Ted Waltman <ted@vafm.org>
Date: Thursday, October 8, 2009 8:01 am
Subject: RE: [rebel-builders] Measuring chord for VG's
To: rebel-builders@dcsol.com
Not being an aerodynamic engineer, why is it always flaps-
up? Wouldn't you
want to optimize VG performance in the typical landing
configuration, e.g.
flaps down? Any information much appreciated.

Ted

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On
Behalf Of Bob
Patterson
Sent: Thursday, October 08, 2009 8:55 AM
To: rebel-builders@dcsol.com
Subject: Re: [rebel-builders] Measuring chord for VG's


Hi Ted !

It's always flaps up - should be the
same as the Rebel = 60 inches.

--
......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 Thursday 08 October 2009 14:35, Ted Waltman wrote:
Are folks measuring chord from wing front to flap-end with the
flaps up or
down?



Anyone know what the chord is of a Super Rebel or Moose (with
flaps up &
flaps down)?



Thanks!



Ted



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mike jones

[rebel-builders] Measuring chord for VG's

Post by mike jones » Sun Feb 19, 2012 5:37 pm

How about some pictures ??

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On Behalf Of Ted
Waltman
Sent: Thursday, October 08, 2009 4:41 PM
To: rebel-builders@dcsol.com
Subject: RE: [rebel-builders] Measuring chord for VG's

Yes, I put them on the h-stab (bottom of course) and the vertical fin. I
suspect the vertical fin install is more useful (designed for?) float
operations?

Ted

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On Behalf Of Jones,
Michael
Sent: Thursday, October 08, 2009 12:47 PM
To: rebel-builders@dcsol.com
Subject: RE: [rebel-builders] Measuring chord for VG's

Has any one put vortex generators on the horizontal or verticla tail
plans ???

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On Behalf Of
David Jackson
Sent: October 8, 2009 2:03 PM
To: Rebel Builders
Subject: RE: [rebel-builders] Measuring chord for VG's

Don't forget what the Vortex generators do - generate vortexs. In order
to do that they have to be outside of the boundary layer airflow to
generate a vortex to break up the boundary layer and move the flow
separation point further back. Moving them further back on a wing just
because it has a longer chord could move them to an area where they are
inside the boundary layer and cannot generate vortexs because there is
not enough airflow over them.



I believe Walter is correct when he says 10% is a start point that the
VG manufacturers use to test. Since we are the manufacturers for our
aircraft we could experiment with different positions to see what works
best. I have read that double-sided tape will hold the VGs in position
well enough for testing purposes but am personally a long way away from
doing that.



Dave J
Date: Thu, 8 Oct 2009 08:16:27 -0700
From: Walter.Klatt@shaw.ca
Subject: Re: RE: [rebel-builders] Measuring chord for VG's
To: rebel-builders@dcsol.com

Ted, I think it is just the way the VG manufacturers do their their
testing and how they define their placement. If you talk to them, I am
sure they will say measure with your flaps in neutral.
They will have different placement recommendations for different types
of planes. 10% is what seems to work best for our wings. I have another
plane with them, and they have to be at the 6 % location to get maximum
benefit. And even then it turned out to only lower stall by about 2 mph,
although it did firm up the ailerons at low speed. The Rebel, on the
other hand, lowered stall by 8 - 10 mph, which is a lot. Also think it
improved climb rate (from my earlier testing with the 320), but that is
very hard to prove. You sure notice the VGs on water take-offs, though.
Walter

----- Original Message -----
From: Ted Waltman <ted@vafm.org>
Date: Thursday, October 8, 2009 8:01 am
Subject: RE: [rebel-builders] Measuring chord for VG's
To: rebel-builders@dcsol.com
Not being an aerodynamic engineer, why is it always flaps-
up? Wouldn't you
want to optimize VG performance in the typical landing
configuration, e.g.
flaps down? Any information much appreciated.

Ted

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On
Behalf Of Bob
Patterson
Sent: Thursday, October 08, 2009 8:55 AM
To: rebel-builders@dcsol.com
Subject: Re: [rebel-builders] Measuring chord for VG's


Hi Ted !

It's always flaps up - should be the
same as the Rebel = 60 inches.

--
......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 Thursday 08 October 2009 14:35, Ted Waltman wrote:
Are folks measuring chord from wing front to flap-end with the
flaps up or
down?



Anyone know what the chord is of a Super Rebel or Moose (with
flaps up &
flaps down)?



Thanks!



Ted



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Ted Waltman

[rebel-builders] Measuring chord for VG's

Post by Ted Waltman » Sun Feb 19, 2012 5:37 pm

I'm waiting on an answer to a couple of questions from the VG folks--Pacific
NW Aero is where I got mine. I'll post their responses and some pics in a
few days. Bug me if I forget <grin>.

Ted

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On Behalf Of mike
jones
Sent: Thursday, October 08, 2009 5:16 PM
To: rebel-builders@dcsol.com
Subject: RE: [rebel-builders] Measuring chord for VG's

How about some pictures ??

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On Behalf Of Ted
Waltman
Sent: Thursday, October 08, 2009 4:41 PM
To: rebel-builders@dcsol.com
Subject: RE: [rebel-builders] Measuring chord for VG's

Yes, I put them on the h-stab (bottom of course) and the vertical fin. I
suspect the vertical fin install is more useful (designed for?) float
operations?

Ted

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On Behalf Of Jones,
Michael
Sent: Thursday, October 08, 2009 12:47 PM
To: rebel-builders@dcsol.com
Subject: RE: [rebel-builders] Measuring chord for VG's

Has any one put vortex generators on the horizontal or verticla tail
plans ???

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On Behalf Of
David Jackson
Sent: October 8, 2009 2:03 PM
To: Rebel Builders
Subject: RE: [rebel-builders] Measuring chord for VG's

Don't forget what the Vortex generators do - generate vortexs. In order
to do that they have to be outside of the boundary layer airflow to
generate a vortex to break up the boundary layer and move the flow
separation point further back. Moving them further back on a wing just
because it has a longer chord could move them to an area where they are
inside the boundary layer and cannot generate vortexs because there is
not enough airflow over them.



I believe Walter is correct when he says 10% is a start point that the
VG manufacturers use to test. Since we are the manufacturers for our
aircraft we could experiment with different positions to see what works
best. I have read that double-sided tape will hold the VGs in position
well enough for testing purposes but am personally a long way away from
doing that.



Dave J
Date: Thu, 8 Oct 2009 08:16:27 -0700
From: Walter.Klatt@shaw.ca
Subject: Re: RE: [rebel-builders] Measuring chord for VG's
To: rebel-builders@dcsol.com

Ted, I think it is just the way the VG manufacturers do their their
testing and how they define their placement. If you talk to them, I am
sure they will say measure with your flaps in neutral.
They will have different placement recommendations for different types
of planes. 10% is what seems to work best for our wings. I have another
plane with them, and they have to be at the 6 % location to get maximum
benefit. And even then it turned out to only lower stall by about 2 mph,
although it did firm up the ailerons at low speed. The Rebel, on the
other hand, lowered stall by 8 - 10 mph, which is a lot. Also think it
improved climb rate (from my earlier testing with the 320), but that is
very hard to prove. You sure notice the VGs on water take-offs, though.
Walter

----- Original Message -----
From: Ted Waltman <ted@vafm.org>
Date: Thursday, October 8, 2009 8:01 am
Subject: RE: [rebel-builders] Measuring chord for VG's
To: rebel-builders@dcsol.com
Not being an aerodynamic engineer, why is it always flaps-
up? Wouldn't you
want to optimize VG performance in the typical landing
configuration, e.g.
flaps down? Any information much appreciated.

Ted

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On
Behalf Of Bob
Patterson
Sent: Thursday, October 08, 2009 8:55 AM
To: rebel-builders@dcsol.com
Subject: Re: [rebel-builders] Measuring chord for VG's


Hi Ted !

It's always flaps up - should be the
same as the Rebel = 60 inches.

--
......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 Thursday 08 October 2009 14:35, Ted Waltman wrote:
Are folks measuring chord from wing front to flap-end with the
flaps up or
down?



Anyone know what the chord is of a Super Rebel or Moose (with
flaps up &
flaps down)?



Thanks!



Ted



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Ken

[rebel-builders] Measuring chord for VG's

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

I put the clear plastic ones on my Rebel stab in the recommended
position and it did nothing. That convinced me that there was not a flow
separation issue with around 27* up elevator. So I increased elevator up
travel to about 30* and that did help, but the VG's are still there as I
haven't got around to removing them. That double sided carpet tape holds
rather well as that was over a year ago and none have fallen off. I
expect no change when I do remove them. Unfortunately with less down
elevator now it does take a bit longer to lift the tail at the start of
takeoff when I'm heavy but that is a minor thing.

I have never felt the need to try them on the rudder but again I have
full rudder travel short of hitting the elevator. Some rebels do not
have the specified 25* of rudder travel. I had to file some material out
of the rudder control horn to get the full 25*.

Ken
R119

Jones, Michael wrote:
Has any one put vortex generators on the horizontal or verticla tail
plans ???

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Walter Klatt

[rebel-builders] Measuring chord for VG's

Post by Walter Klatt » Sun Feb 19, 2012 5:37 pm

Ken, did you put the VGs on the wings, too? I am just curious if anyone has
put them on wings with the STOL kit, and what the effect was.

Walter

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On Behalf Of Ken
Sent: October 9, 2009 1:51 PM
To: rebel-builders@dcsol.com
Subject: Re: [rebel-builders] Measuring chord for VG's

I put the clear plastic ones on my Rebel stab in the recommended
position and it did nothing. That convinced me that there was not a flow
separation issue with around 27* up elevator. So I increased elevator up
travel to about 30* and that did help, but the VG's are still there as I
haven't got around to removing them. That double sided carpet tape holds
rather well as that was over a year ago and none have fallen off. I
expect no change when I do remove them. Unfortunately with less down
elevator now it does take a bit longer to lift the tail at the start of
takeoff when I'm heavy but that is a minor thing.

I have never felt the need to try them on the rudder but again I have
full rudder travel short of hitting the elevator. Some rebels do not
have the specified 25* of rudder travel. I had to file some material out
of the rudder control horn to get the full 25*.

Ken
R119

Jones, Michael wrote:
Has any one put vortex generators on the horizontal or verticla tail
plans ???

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Jim Cole

[rebel-builders] Measuring chord for VG's

Post by Jim Cole » Sun Feb 19, 2012 5:37 pm

I have Pierre's old wings (up in the rafters) with the VG's and stol kit but
never flew it. Bob Patterson did so he can probably comment.

Cheers
Jim


On 10/9/09 8:05 PM, "Walter Klatt" <Walter.Klatt@shaw.ca> wrote:
Ken, did you put the VGs on the wings, too? I am just curious if anyone has
put them on wings with the STOL kit, and what the effect was.

Walter

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On Behalf Of Ken
Sent: October 9, 2009 1:51 PM
To: rebel-builders@dcsol.com
Subject: Re: [rebel-builders] Measuring chord for VG's

I put the clear plastic ones on my Rebel stab in the recommended
position and it did nothing. That convinced me that there was not a flow
separation issue with around 27* up elevator. So I increased elevator up
travel to about 30* and that did help, but the VG's are still there as I
haven't got around to removing them. That double sided carpet tape holds
rather well as that was over a year ago and none have fallen off. I
expect no change when I do remove them. Unfortunately with less down
elevator now it does take a bit longer to lift the tail at the start of
takeoff when I'm heavy but that is a minor thing.

I have never felt the need to try them on the rudder but again I have
full rudder travel short of hitting the elevator. Some rebels do not
have the specified 25* of rudder travel. I had to file some material out
of the rudder control horn to get the full 25*.

Ken
R119

Jones, Michael wrote:
Has any one put vortex generators on the horizontal or verticla tail
plans ???

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Ken

[rebel-builders] Measuring chord for VG's

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

No I didn't put them on the wings Walter.
Angus bought a set to try with his STOL cuff but he had not tried them
yet as of a few weeks ago. I don't see how the ability to fly at an even
higher angle of attack can possibly help but hey it's all fun and
learning ;)

Odd that I've never noticed VG's on any of the dehavilland Beaver or
Otter aircraft?? I would have thought they might be a natural for VG's
with the 4415 wing and a lot more flap than we have...

Ken

Walter Klatt wrote:
Ken, did you put the VGs on the wings, too? I am just curious if anyone has
put them on wings with the STOL kit, and what the effect was.

Walter

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Walter Klatt

[rebel-builders] Measuring chord for VG's

Post by Walter Klatt » Sun Feb 19, 2012 5:37 pm

Yeah, when you talk to aeronautical engineers and designers, they still take
the view that VGs are only necessary to correct a flaw. The Beavers, and
Otters even more so, have very long wings compared to ours, so maybe VGs
don't do much for them.

To me they are still a black science. I used to believe that it was all just
about angle of attack, but since flying with them on floats for a few years
now, there is no doubt in my mind they create extra lift even without a high
angle of attack. They also really help lift off (and land) a very heavily
loaded plane, too. And I see how well the Elite (150 pounds more than a
Rebel) with them performs off the water.

I was out at the lake today, and came back to a 10 kt gusting 20, 90 degree
crosswind at Langley. That is not common here actually, and I don't get a
lot of crosswind practice. But despite having to really work the ailerons in
the gusts to keep the wing down and almost full rudder, it was almost easy
to softly touch down one wheel first, and even gently lower the front ones
as I normally do in low wind conditions. I truly think it is the VGs that
help in these situations, and keep those flaperons responsive even at slower
speeds. I found out later that a Cessna pranged up on landing a little
earlier.

Anyway, as everyone here well knows by now, I am definitely a VG fan.

Walter

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On Behalf Of Ken
Sent: October 9, 2009 6:18 PM
To: rebel-builders@dcsol.com
Subject: Re: [rebel-builders] Measuring chord for VG's

No I didn't put them on the wings Walter.
Angus bought a set to try with his STOL cuff but he had not tried them
yet as of a few weeks ago. I don't see how the ability to fly at an even
higher angle of attack can possibly help but hey it's all fun and
learning ;)

Odd that I've never noticed VG's on any of the dehavilland Beaver or
Otter aircraft?? I would have thought they might be a natural for VG's
with the 4415 wing and a lot more flap than we have...

Ken

Walter Klatt wrote:
Ken, did you put the VGs on the wings, too? I am just curious if anyone
has
put them on wings with the STOL kit, and what the effect was.

Walter

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Bob Patterson

[rebel-builders] Measuring chord for VG's

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

Oh, well.... allright ! :-)

It was a long time ago, but I was very impressed with that wing.
It would fly at crazy angles, and, if you snuck up on it gently,
you could fly around with the throttle closed and the stick
all the way back, solid as a rock, sinking about 400 fpm,
with full aileron control ! Even rolling into steep turns
one way, then the other - no inclination to fall off & spin.

Thought that was a handy safety tool, if ever stuck 'on top' -
just set it up like that, and come down through the tiniest hole,
or go straight ahead, and make your own .... ;-)

That Rebel had everything - Fife Horner wing tips, McKenzie
STOL kit, with cuff & wing fences, and VG's !!

--
......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 Saturday 10 October 2009 00:09, Jim Cole wrote:
I have Pierre's old wings (up in the rafters) with the VG's and stol kit
but never flew it. Bob Patterson did so he can probably comment.

Cheers
Jim

On 10/9/09 8:05 PM, "Walter Klatt" <Walter.Klatt@shaw.ca> wrote:
Ken, did you put the VGs on the wings, too? I am just curious if anyone
has put them on wings with the STOL kit, and what the effect was.

Walter

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On Behalf Of
Ken Sent: October 9, 2009 1:51 PM
To: rebel-builders@dcsol.com
Subject: Re: [rebel-builders] Measuring chord for VG's

I put the clear plastic ones on my Rebel stab in the recommended
position and it did nothing. That convinced me that there was not a flow
separation issue with around 27* up elevator. So I increased elevator up
travel to about 30* and that did help, but the VG's are still there as I
haven't got around to removing them. That double sided carpet tape holds
rather well as that was over a year ago and none have fallen off. I
expect no change when I do remove them. Unfortunately with less down
elevator now it does take a bit longer to lift the tail at the start of
takeoff when I'm heavy but that is a minor thing.

I have never felt the need to try them on the rudder but again I have
full rudder travel short of hitting the elevator. Some rebels do not
have the specified 25* of rudder travel. I had to file some material out
of the rudder control horn to get the full 25*.

Ken
R119

Jones, Michael wrote:
Has any one put vortex generators on the horizontal or verticla tail
plans ???



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Rob Luce

[rebel-builders] Measuring chord for VG's

Post by Rob Luce » Sun Feb 19, 2012 5:37 pm

The plane on 733 is to put VG's on it, but that's a ways down the road, so we haven't debated the subject heavily.

I find the black science comment somewhat funny. VG's are one of the easiest things to document in a low wing aircraft. A roll of tape, a ball of yarn, and a video camera, go flying and take before and after videos. It's fairly plain to see. Youtube has a number of video's of people trying out low wing aircraft with VG's.

I put VG's on a '66 172, made a huge difference on landing. Crosswind or heavy winds, the controls were simply alot more effective to slower speeds. The VG's made it a much safer plane in nearly any instance. Let's just say it did add a touch of drag. In a 172 or Rebel? Who cares.

I never saw any difference in top end speed due to the VG's in the 172, O-300 or O-360. But low speed, it was dramatic.

If you're in a Lancair or RV, there's probably more to debate. In anything less than 150 kts, the debate is probably meaningless.

Rob Luce
R733




________________________________
From: Walter Klatt <Walter.Klatt@shaw.ca>
To: rebel-builders@dcsol.com
Sent: Fri, October 9, 2009 8:49:29 PM
Subject: RE: [rebel-builders] Measuring chord for VG's

Yeah, when you talk to aeronautical engineers and designers, they still take
the view that VGs are only necessary to correct a flaw. The Beavers, and
Otters even more so, have very long wings compared to ours, so maybe VGs
don't do much for them.

To me they are still a black science. I used to believe that it was all just
about angle of attack, but since flying with them on floats for a few years
now, there is no doubt in my mind they create extra lift even without a high
angle of attack. They also really help lift off (and land) a very heavily
loaded plane, too. And I see how well the Elite (150 pounds more than a
Rebel) with them performs off the water.

I was out at the lake today, and came back to a 10 kt gusting 20, 90 degree
crosswind at Langley. That is not common here actually, and I don't get a
lot of crosswind practice. But despite having to really work the ailerons in
the gusts to keep the wing down and almost full rudder, it was almost easy
to softly touch down one wheel first, and even gently lower the front ones
as I normally do in low wind conditions. I truly think it is the VGs that
help in these situations, and keep those flaperons responsive even at slower
speeds. I found out later that a Cessna pranged up on landing a little
earlier.

Anyway, as everyone here well knows by now, I am definitely a VG fan.

Walter

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On Behalf Of Ken
Sent: October 9, 2009 6:18 PM
To: rebel-builders@dcsol.com
Subject: Re: [rebel-builders] Measuring chord for VG's

No I didn't put them on the wings Walter.
Angus bought a set to try with his STOL cuff but he had not tried them
yet as of a few weeks ago. I don't see how the ability to fly at an even
higher angle of attack can possibly help but hey it's all fun and
learning ;)

Odd that I've never noticed VG's on any of the dehavilland Beaver or
Otter aircraft?? I would have thought they might be a natural for VG's
with the 4415 wing and a lot more flap than we have...

Ken

Walter Klatt wrote:
Ken, did you put the VGs on the wings, too? I am just curious if anyone
has
put them on wings with the STOL kit, and what the effect was.

Walter

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