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Winglts ?
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Lew Gallagher



Joined: 04 Jan 2008
Posts: 402
Location: Greenville , SC

PostPosted: Thu Jul 16, 2009 5:10 am    Post subject: Winglts ? Reply with quote

Hey guys,

I've been thinking about this for awhile and thought I'd air it out -- especially now that many of you might check it out at Osh with the vendors.

What do you think of winglets instead of just wingtips? Supposedly they create a better vortex, enhance lift ... ? I dunno, but now I see them in the magazines (Plane & Pilot) on the new Diamonds and Cessna 400 etc. -- not just the big commercial planes.

From a builder's point of view, is it just as easy to fit a winglet as a wingtip?, stress/structure issues?, would they change flying/handling? how to engineer them for the -10?

I read here about counting ounces and fine tuning everything from injectors to positioning antennas to tweak the most out of efficiency, reducing drag, etc. ... winglets would seem to be an obvious area to look into.

Whatcha think?

Later, - Lew


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orchidman



Joined: 10 Jul 2006
Posts: 277
Location: Oklahoma City - KRCE

PostPosted: Thu Jul 16, 2009 6:39 am    Post subject: Re: Winglts ? Reply with quote

I asked this question in the Vans tent 2 years ago and was blown off because they didn't think it would add any significant performance. Something about having relatively short wings.

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johngoodman



Joined: 18 Sep 2006
Posts: 530
Location: GA

PostPosted: Thu Jul 16, 2009 6:48 am    Post subject: Re: Winglts ? Reply with quote

You need a big wing before it really makes any difference, and it's minor at that.
John


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PostPosted: Thu Jul 16, 2009 6:53 am    Post subject: Winglts ? Reply with quote

There was a great discussion of winglets on the Lancair Mail List a few weeks ago.  What I took from it was that winglets improve efficiency at high angles of attack:  take-off, climb, landing, and very high altitude cruise.  Perfect for airliners and pressurized GA planes but not so helpful for planes like RVs.  At low angles of attack, where RVs excel, winglets would most likely slow the plane down.

Plus, there's a lot of engineering and testing that goes into a winglet--they aren't a simple bolt-on.  The angles and airfoils are critical.  I understand the airlines use them to gain tiny efficiencies that pay off over millions of miles.

Dave

On Thu, Jul 16, 2009 at 6:10 AM, Lew Gallagher <lewgall(at)charter.net (lewgall(at)charter.net)> wrote:
Quote:
--> RV10-List message posted by: "Lew Gallagher" <lewgall(at)charter.net (lewgall(at)charter.net)>

Hey guys,

I've been thinking about this for awhile and thought I'd air it out -- especially now that many of you might check it out at Osh with the vendors.

What do you think of winglets instead of just wingtips?  Supposedly they create a better vortex, enhance lift ... ?  I dunno, but now I see them in the magazines (Plane & Pilot) on the new Diamonds and Cessna 400 etc. -- not just the big commercial planes.

>From a builder's point of view, is it just as easy to fit a winglet as a wingtip?, stress/structure issues?, would they change flying/handling?  how to engineer them for the -10?

I read here about counting ounces and fine tuning everything from injectors to positioning antennas to tweak the most out of efficiency, reducing drag, etc.  ... winglets would seem to be an obvious area to look into.

Whatcha think?

Later, - Lew

--------
non-pilot
crazy about building
NOW OFICIALLY BUILDER #40549
Painting done!
On with wiring and avionics.




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N520TX



Joined: 13 Oct 2008
Posts: 9

PostPosted: Thu Jul 16, 2009 6:54 am    Post subject: Winglts ? Reply with quote

A neighbor of mine hosted a rotary engine fly-in a couple months ago. There
was a guy there that has a custom fiberglass molding business - he brought a
pair of what are called "finch-tips". These are tips where the outboard edge
sweeps down and rearward. They only fit the 4/6/7/9 currently and he was
looking for someone to test fly them to gather numbers.

I did the work to install them on my 7a and have flown them twice so far.
The stall speeds are unchanged, but in my trials so far, I've seen that the
mid-power range speeds are improved by about 7mph. I'm far from complete
with my flight testing, but they are showing promise. I have photo's posted
on my picasa page - http://picasaweb.google.com/n520tx/NewWingtips#.

When I get all my testing done, I plan to post up the final numbers on my
web site.

For what it's worth ...

Ron

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PostPosted: Thu Jul 16, 2009 8:15 am    Post subject: Winglts ? Reply with quote

Ron,
Thanks for the post. The tip looked like a pretty good match for
a prototype. It's funny how ego plays a part in these things. The exact
same wing tip flipped up has some marketing potential but a turned down
winglet much like the old Cherokee wing tips are more of an eyesore (to
my design sensibilities). Regardless please keep us informed of your
test results.

Robin
--


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PostPosted: Thu Jul 16, 2009 10:43 am    Post subject: Winglts ? Reply with quote

That, and the fact that the wing is 'Hershey bar' shape. I think
winglets would be far more efficient on a swept wing.
Linn

orchidman wrote:
Quote:


I asked this question in the Vans tent 2 years ago and was blown off because they didn't think it would add any significant performance. Something about having relatively short wings.

--------
Gary Blankenbiller
RV10 - # 40674
(N2GB Flying)


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PostPosted: Thu Jul 16, 2009 11:14 am    Post subject: Winglts ? Reply with quote

Well, I kinda like the droop tips on the Cherokee. Klingon warship
comes to mind. I think the droop style would help the low speed stall
far more than a swept up winglet. The droop tips on the Cherokee really
do make a short field landing far shorter!!!
Linn

Robin Marks wrote:
Quote:


Ron,
Thanks for the post. The tip looked like a pretty good match for
a prototype. It's funny how ego plays a part in these things. The exact
same wing tip flipped up has some marketing potential but a turned down
winglet much like the old Cherokee wing tips are more of an eyesore (to
my design sensibilities). Regardless please keep us informed of your
test results.

Robin



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PostPosted: Thu Jul 16, 2009 11:16 am    Post subject: Winglts ? Reply with quote

Anyone using other than Cleveland brakes mine are getting hot and
wearing out too fast.any other brakes recommended or being used?

Sent from my iPhone

Robert E. Brunkenhoefer
Brunkenhoefer Law Firm, P.C.
520 Lawrence St.
Corpus Christi, Texas 78401
Phone: 361-888-8808
Facsimile: 361-888-6753
robert(at)brunklaw.com

On Jul 16, 2009, at 1:41 PM, Linn Walters <pitts_pilot(at)bellsouth.net>
wrote:

Quote:

>

That, and the fact that the wing is 'Hershey bar' shape. I think
winglets would be far more efficient on a swept wing.
Linn

orchidman wrote:
>
>
> I asked this question in the Vans tent 2 years ago and was blown
> off because they didn't think it would add any significant
> performance. Something about having relatively short wings.
>
> --------
> Gary Blankenbiller
> RV10 - # 40674
> (N2GB Flying)
>
>
> Read this topic online here:
>
> http://forums.matronics.com/viewtopic.php?p 53329#253329
>
>


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AV8ORJWC



Joined: 13 Jul 2006
Posts: 1149
Location: Aurora, Oregon "Home of VANS"

PostPosted: Thu Jul 16, 2009 12:25 pm    Post subject: Winglts ? Reply with quote

The larger mass of an upgraded rotor can assist cooling as can a larger
caliper. The technical support at Cleveland can assist in beginning
with their parts used and larger upgrades. Tim James did a great job
with OEM Cessna. There is also Beringer. Beyond the benefit of cooler
temperatures is the shorter stopping distance at the same speed and same
weight. Don't forget to think about a fluid upgrade as H-5606 is more
combustible than alternatives. Once a brake line leaks the chain
reaction begins.

John Cox
,
--


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AV8ORJWC



Joined: 13 Jul 2006
Posts: 1149
Location: Aurora, Oregon "Home of VANS"

PostPosted: Thu Jul 16, 2009 12:28 pm    Post subject: Winglts ? Reply with quote

VGs also help the slow speed characteristics without shocking the design
sensibilities of a few readers. What one calls a winglet might not
reach the NACA standard, but might be just another unique wing tip
design.

New ideas are always a fresh perspective with OSH just around the
corner.

John Cox

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PostPosted: Thu Jul 16, 2009 1:05 pm    Post subject: Winglts ? Reply with quote

are you using this upgrade on your rv10?
On Jul 16, 2009, at 3:24 PM, John Cox wrote:

[quote]

The larger mass of an upgraded rotor can assist cooling as can a
larger
caliper. The technical support at Cleveland can assist in beginning
with their parts used and larger upgrades. Tim James did a great job
with OEM Cessna. There is also Beringer. Beyond the benefit of cooler
temperatures is the shorter stopping distance at the same speed and
same
weight. Don't forget to think about a fluid upgrade as H-5606 is more
combustible than alternatives. Once a brake line leaks the chain
reaction begins.

John Cox
,
--


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AV8ORJWC



Joined: 13 Jul 2006
Posts: 1149
Location: Aurora, Oregon "Home of VANS"

PostPosted: Thu Jul 16, 2009 1:48 pm    Post subject: Winglts ? Reply with quote

Robert,

I am going with 0.375" thick rotors and dual pad calipers per side to
spread the force. A couple of RV-x main landing gear caliper fires that
consumed the glass pant caused a few to change from H-5606 a few years
back. The flame propagation was right below each main AVGAS fuel tank.
Fiberglass fires are a perverted thing to watch. So take a test sample
and learn by experiment not experience how the cured resin and glass
strands come to life until gone. Mine was watching a '69 Vette being
prepped for custom paint.

VANS mantra is stay conservative with the brakes and build your kit bone
stock. Some of us tend to lean into the wind - just for the fresh sea
breeze in the summer. With a Barrett and Forsling Exhaust, the brake
upgrade was an easy choice. Ask about VGs for the RV-10 at OSH.

Mil H-83282 provides another level of combustion protection. I have
found that H-5606 tends to coagulate with age. Its low flash point is
routinely accepted by most builders without consideration of
alternatives.

Some will yell "Stay off the brakes and learn Happy Feet". Then your
neighborhood A&P will explain how proper engine leaning and a higher
idle than 700 or 800 will cause the aircraft to move in a forward
direction requiring those darned toes again.

Fly Often, Fly Safe, Earn your grey hair over time. Take a Grandchild
for a Young Eagles flight. Stop by Camp Condrey for a beer.

John

--


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Kelly McMullen



Joined: 16 Apr 2008
Posts: 1188
Location: Sun Lakes AZ

PostPosted: Thu Jul 16, 2009 1:48 pm    Post subject: Winglts ? Reply with quote

IIRC the blended airfoil winglets on B7x7 aircraft account for 3-4% fuel economy as well as lowered stall speed, etc. There are droop wingtips for aircraft such as hersey bar Cherokees and C172s that apparently are effective for stall reduction without too much drag addition.

On Thu, Jul 16, 2009 at 7:52 AM, Dave Saylor <dave.saylor.aircrafters(at)gmail.com (dave.saylor.aircrafters(at)gmail.com)> wrote:
[quote] There was a great discussion of winglets on the Lancair Mail List a few weeks ago.  What I took from it was that winglets improve efficiency at high angles of attack:  take-off, climb, landing, and very high altitude cruise.  Perfect for airliners and pressurized GA planes but not so helpful for planes like RVs.  At low angles of attack, where RVs excel, winglets would most likely slow the plane down.

Plus, there's a lot of engineering and testing that goes into a winglet--they aren't a simple bolt-on.  The angles and airfoils are critical.  I understand the airlines use them to gain tiny efficiencies that pay off over millions of miles.

Dave
[b]


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PostPosted: Thu Jul 16, 2009 3:50 pm    Post subject: Winglts ? Reply with quote

Thanks for the help. Where do I get the parts and how much has to be
done to the fairings brackets to make the upgrade fit

Sent from my iPhone

Robert E. Brunkenhoefer
Brunkenhoefer Law Firm, P.C.
520 Lawrence St.
Corpus Christi, Texas 78401
Phone: 361-888-8808
Facsimile: 361-888-6753
robert(at)brunklaw.com

On Jul 16, 2009, at 4:46 PM, "John Cox" <johnwcox(at)pacificnw.com> wrote:

[quote] Robert,

I am going with 0.375" thick rotors and dual pad calipers per side to
spread the force. A couple of RV-x main landing gear caliper fires
that
consumed the glass pant caused a few to change from H-5606 a few years
back. The flame propagation was right below each main AVGAS fuel tank.
Fiberglass fires are a perverted thing to watch. So take a test sample
and learn by experiment not experience how the cured resin and glass
strands come to life until gone. Mine was watching a '69 Vette being
prepped for custom paint.

VANS mantra is stay conservative with the brakes and build your kit
bone
stock. Some of us tend to lean into the wind - just for the fresh sea
breeze in the summer. With a Barrett and Forsling Exhaust, the brake
upgrade was an easy choice. Ask about VGs for the RV-10 at OSH.

Mil H-83282 provides another level of combustion protection. I have
found that H-5606 tends to coagulate with age. Its low flash point is
routinely accepted by most builders without consideration of
alternatives.

Some will yell "Stay off the brakes and learn Happy Feet". Then your
neighborhood A&P will explain how proper engine leaning and a higher
idle than 700 or 800 will cause the aircraft to move in a forward
direction requiring those darned toes again.

Fly Often, Fly Safe, Earn your grey hair over time. Take a Grandchild
for a Young Eagles flight. Stop by Camp Condrey for a beer.

John

--


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PostPosted: Thu Jul 16, 2009 6:23 pm    Post subject: Winglts ? Reply with quote

This is a first for me. I've used Cleveland brakes almost my whole
flying life, and find them better than the alternatives. My only guess
is that you ride the brakes while taxiing (give the brakes a tap or two
to keep the nose pointed to where you want to go rather than constant
pressure) ...... or your brakes don't relax when you release them. I'd
check to make sure the brake cylinder rides on the pins freely. They
don't need lubrication, which usually just gums them up and attracts
dirt. Are the pads wearing evenly??? Uneven wear is a sign of the
brake cylinder hanging up on the pins, or a mounting problem. Improper
break-in could also be a cause.
Linn

Robert Brunkenhoefer wrote:
Quote:

<rebrunk42(at)gmail.com>

Anyone using other than Cleveland brakes mine are getting hot and
wearing out too fast.any other brakes recommended or being used?

Sent from my iPhone

Robert E. Brunkenhoefer
Brunkenhoefer Law Firm, P.C.
520 Lawrence St.
Corpus Christi, Texas 78401
Phone: 361-888-8808
Facsimile: 361-888-6753
robert(at)brunklaw.com


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PostPosted: Thu Jul 16, 2009 6:40 pm    Post subject: Winglts ? Reply with quote

Yes I'll admit it, I would not add drop down winglets to my -10 if it
added 15 more knots in cruise and washed itself when it was dirty.
That being said... John have you seen the clear rubberized VG's on the
Cessna Columbia's leading edge? Small in profile and difficult to see
unless you are either looking for them or right up against the wing.
Also interesting because they are on the forward most portion of the
leading edge vs. typical VG's further up the curvature of the wing.
Interesting item.
I thought that one could design and mold them in 18" sections and just
link end to end. Then I remembered that one would have to conduct proper
R&D first. Oh that.....

Robin

--


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AV8ORJWC



Joined: 13 Jul 2006
Posts: 1149
Location: Aurora, Oregon "Home of VANS"

PostPosted: Thu Jul 16, 2009 8:29 pm    Post subject: Winglts ? Reply with quote

Tim James #623 has done a major improvement in both handling and low
speed flight with his VGs. Others might query at OSH and post their
impressions here.

The 10 can provide some great, short, soft, H DenAlt landings and
unimproved surfaces with a few reasonably simple mods.

For many who never leave the asphalt jungle, I understand.

John

--


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Kelly McMullen



Joined: 16 Apr 2008
Posts: 1188
Location: Sun Lakes AZ

PostPosted: Fri Jul 17, 2009 4:14 am    Post subject: Winglts ? Reply with quote

Unfortunately, VGs benefits come at a cost of reduced cruise speed. Depends on airfoil and max speed range. I would not be surprised to see a loss of 3-5 kts from cruise. Fine if you main mission is back country, not so good if you mainly fly cross country.

On Thu, Jul 16, 2009 at 9:26 PM, John Cox <johnwcox(at)pacificnw.com (johnwcox(at)pacificnw.com)> wrote:
[quote] --> RV10-List message posted by: "John Cox" <johnwcox(at)pacificnw.com (johnwcox(at)pacificnw.com)>


Tim James #623 has done a major improvement in both handling and low
speed flight with his VGs.  Others might query at OSH and post their
impressions here.

The 10 can provide some great, short, soft, H DenAlt landings and
unimproved surfaces with a few reasonably simple mods.

For many who never leave the asphalt jungle, I understand.

John

--


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A&P/IA, EAA Tech Counselor
KCHD
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PostPosted: Fri Jul 17, 2009 6:13 am    Post subject: Winglts ? Reply with quote

Thanks for the info I will try and check those items. Robert n661g
130hrs

Sent from my iPhone

Robert E. Brunkenhoefer
Brunkenhoefer Law Firm, P.C.
520 Lawrence St.
Corpus Christi, Texas 78401
Phone: 361-888-8808
Facsimile: 361-888-6753
robert(at)brunklaw.com

On Jul 16, 2009, at 9:21 PM, Linn Walters <pitts_pilot(at)bellsouth.net>
wrote:

Quote:

>

This is a first for me. I've used Cleveland brakes almost my whole
flying life, and find them better than the alternatives. My only
guess is that you ride the brakes while taxiing (give the brakes a
tap or two to keep the nose pointed to where you want to go rather
than constant pressure) ...... or your brakes don't relax when you
release them. I'd check to make sure the brake cylinder rides on
the pins freely. They don't need lubrication, which usually just
gums them up and attracts dirt. Are the pads wearing evenly???
Uneven wear is a sign of the brake cylinder hanging up on the pins,
or a mounting problem. Improper break-in could also be a cause.
Linn

Robert Brunkenhoefer wrote:
>
> >
>
> Anyone using other than Cleveland brakes mine are getting hot and
> wearing out too fast.any other brakes recommended or being used?
>
> Sent from my iPhone
>
> Robert E. Brunkenhoefer
> Brunkenhoefer Law Firm, P.C.
> 520 Lawrence St.
> Corpus Christi, Texas 78401
> Phone: 361-888-8808
> Facsimile: 361-888-6753
> robert(at)brunklaw.com



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