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Cabin airfoil
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stepinwolf



Joined: 21 Jan 2008
Posts: 133
Location: Canada

PostPosted: Fri Jan 25, 2008 4:27 pm    Post subject: Cabin airfoil Reply with quote

Has anyone built up the section over the cabin as an airfoil, in the same shape as the wing. I'm not planning to do much flying while looking though the skylight, so I am thinking that by building it in this way, I would have an additional 16 to 17 sq. feet of wing area, not to mention another 4.5' section of slats.

Thanks to those of you, who will take the time to respond to my request for information.

Bob, the 701 scratch


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PostPosted: Fri Jan 25, 2008 5:06 pm    Post subject: Cabin airfoil Reply with quote

Quote:
I think the "Savanah" has a straight wing instead
of the break in the middle...do not archive....
--- stepinwolf <robert.pelland(at)cgocable.ca> wrote:


Quote:

<robert.pelland(at)cgocable.ca>

Has anyone built up the section over the cabin as an
airfoil, in the same shape as the wing. I'm not
planning to do much flying while looking though the
skylight, so I am thinking that by building it in
this way, I would have an additional 16 to 17 sq.
feet of wing area, not to mention another 4.5'
section of slats.

Thanks to those of you, who will take the time to
respond to my request for information.

Bob, the 701 scratch

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kmccune



Joined: 22 Sep 2007
Posts: 577
Location: Wisconsin, USA

PostPosted: Fri Jan 25, 2008 8:31 pm    Post subject: Re: Cabin airfoil Reply with quote

I have heard of others doing this, one I believe to be quite knowledgeable . But I just can not see how you can get any lift from this. There is no bottom of the airfoil.

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stepinwolf



Joined: 21 Jan 2008
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PostPosted: Sat Jan 26, 2008 3:10 am    Post subject: Re: Cabin airfoil Reply with quote

Kevin, thanks for your input.

I am in no way an engineer, but I always thought that lift was created by the low pressure area on top of the wing. If we look at most of the light aircraft on the market today, they all seem to have an airfoil over the top of cabin area, so I'm guessing it has to be a factor in the overall performance of the wing.

Bob


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PostPosted: Sat Jan 26, 2008 4:26 am    Post subject: Cabin airfoil Reply with quote

You are partially correct. The rest of the story is the realtively higher airpressure under the corresponding undersurface of the plane (the fuselage in this discussion). The differential produces your lift. Both the shape of the airfoil and the AOA are factors in producing lift.

Dred
[quote] ---


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kmccune



Joined: 22 Sep 2007
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PostPosted: Sat Jan 26, 2008 4:49 am    Post subject: Re: Cabin airfoil Reply with quote

This is my thought too. The shorter path underneath is just as important as the top shape. You may get lift right as the sides of the cabin were the standard wing tapers down. And it would seem to reduce drag. But you would lose the prop wash on the rear at low speeds. Though the Savannah seems to do just fine with this section over the roof.

My guess is that it just looks nice this way. Early high wing airplanes were all open so there was lift in this area. When they put the cabin on, they simply set the wing on top of it. ( total conjecture on my part by the way :_) )
Some designs also have a tube running the full span acting as the main spar. This kind of forces the shape over the cabin.
There may still be lift there, but I like I said I have no idea how it would work.


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PostPosted: Sat Jan 26, 2008 5:54 am    Post subject: Cabin airfoil Reply with quote

This explains a lot about wings, and airfoils. It appears to be a complex
subject. http://www.regenpress.com/


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PostPosted: Sat Jan 26, 2008 6:36 am    Post subject: Cabin airfoil Reply with quote

Kevin,

A lot of our list posters seem to have bought into the premise that an airplane flies because of the lift provided by the Bernoulli effect of the upper surface of the wing. In fact, most of the lift is provided by Newton, pushing on the bottom surface of the wing (With enough power, you can fly a barn door). This speaks very loudly about the "expertise" of some of our most prolific posters, right?

Jay in Dallas
"kmccune" <kmccune(at)somtel.net> wrote:

Quote:


I have heard of others doing this, one I believe to be quite knowledgeable . But I just can not see how you can get any lift from this. There is no bottom of the airfoil.

--------
Kevin
N701DZ Reserved


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PostPosted: Sat Jan 26, 2008 6:47 am    Post subject: Cabin airfoil Reply with quote

Bob and Kevin, I am by no means an expert in
aerodynamics so take this with a grain of salt.

Chris Hientz is the master of form follows function.
He did the wings on the 701 the way he did for one
reason for sure, in a high angle of bank, your
visability out the top will be much better because of
the thinner wing profile at the root. Additionally,
there has been some mention on this group of prop
blast to the tail feathers through the opening. I
can't comment on that one but it at least makes sense.

As a comparison, I checked out a Land Africa (rip off
of a rip off of a 701)that a friend of mine was
helping to build. It had the airfoil shape over the
cabin. While the Land Africa has a really nice three
angle instrument panel, the cabin top was kind of ugly
in my eyes. I know, beauty is not something that
whould be used in the same e-mail as anything about a
701. In all honesty, the change to the cabin looked
to me like it was done to simplify construction of the
wing roots more than provide additional lift. Lets
face it, fitting those wing roots on the 701 looks
like a bit of a challenge. I'll see when I get there
in a couple of months.

As for the amount of lift created by the one sided
airfoil, I can explain that a bit. First, this
information come from the ground school lectures that
I teach to the youth group I work with. It comes from
their lesson plans and from the ASA ground school DVD
I use as a basis for my lessons. I am sure there are
more knowledgable people on this list than me that
will fill in the blanks if I am incorrect on my
impressions.

Lift on an airfoil can be broken down into two main
parts. The first part is called (I think) Plate Lift
and is the effect of the relative wind hitting the
bottom of the wing. Same idea as sticking your hand
out the window of a car going down the highway. If I
understand my aerodynamics correctly, this part of the
lift makes up about 60% if the total lift generated by
a wing. The other 40% is made up by the air being
accellerated over the top of the wing and creating low
pressure ala Bernoulli.

So, providing my understanding of aerodynamic
principals is accurate, you will not gain much by
adding the 4 ft of span to the airfoil shape.
Especially if the interference of the rear fuselage
has any effect of the efficiency of the airflow over
the airfoil shape. The big advantage would be not
having to build the tapered wing root.

Again, if someone has a better understanding of this
than me, feel free to straighten us all out.

Doug MacDonald
CH-701 Scratch Builder
NW Ontario, Canada

Quote:

<robert.pelland(at)cgocable.ca>

Kevin, thanks for your input.

I am in no way an engineer, but I always thought
that lift was created by the low pressure area on
top of the wing. If we look at most of the light
aircraft on the market today, they all seem to have
an airfoil over the top of cabin area, so I'm
guessing it has to be a factor in the overall
performance of the wing.

Bob

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PostPosted: Sat Jan 26, 2008 7:22 am    Post subject: Cabin airfoil Reply with quote

I stand correct............
---


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PostPosted: Sat Jan 26, 2008 7:26 am    Post subject: Cabin airfoil Reply with quote

Bernoulli ?
Ever watch a DC 9 take off?
Short wings and carries 137 people PLUS baggage.....
There is a lot of Bernoulli happening........Not!
---


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PostPosted: Sat Jan 26, 2008 7:44 am    Post subject: Cabin airfoil Reply with quote

One thing not mentioned is the increased headroom for those who might need
or want it. The other is the using of the term "rip off". I remind every
one that the 701 is in fact a copy of a multitude of parts used by
previously like aircraft, by no means is it an original design. I would
never say it's a rip off, it's just smart engineering of proven concepts and
parts, as is the Savanna.

LRM, skyhawg.com.
---


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PostPosted: Sat Jan 26, 2008 7:45 am    Post subject: Cabin airfoil Reply with quote

But to get the barn door to fly it must be at an angle to the air flow. Thus the air flow over the door will appear to be an airfoil. Jerry of Ga

In a message dated 1/26/2008 9:37:18 A.M. Eastern Standard Time, Jaybannist(at)cs.com writes:
Quote:
--> Zenith-List message posted by: Jaybannist(at)cs.com

Kevin,

A lot of our list posters seem to have bought into the premise that an airplane flies because of the lift provided by the Bernoulli effect of the upper surface of the wing. In fact, most of the lift is provided by Newton, pushing on the bottom surface of the wing (With enough power, you can fly a barn door). This speaks very loudly about the "expertise" of some of our most prolific posters, right?

Jay in Dallas
"kmccune" <kmccune(at)somtel.net> wrote:

Quote:
--> Zenith-List message posted by: "kmccune" <kmccune(at)somtel.net>

I have heard of others doing this, one I believe to be quite knowledgeable . But I just can not see how you can get any lift from this. There is no bottom of the airfoil.

--------
Kevin
N701DZ Reserved


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PostPosted: Sat Jan 26, 2008 8:10 am    Post subject: Cabin airfoil Reply with quote

Also true. For anyone really interested in the lift theory, there is an excellent (and long) item on the subject at www.eskimo.com/~billb/wing/airfoil.html. The true/false session at the end is the most informative.

Jay in Dallas
Jeyoung65(at)aol.com wrote:

Quote:
But to get the barn door to fly it must be at an angle to the air flow. Thus
the air flow over the door will appear to be an airfoil. Jerry of Ga


In a message dated 1/26/2008 9:37:18 A.M. Eastern Standard Time,
Jaybannist(at)cs.com writes:



Kevin,

A lot of our list posters seem to have bought into the premise that an
airplane flies because of the lift provided by the Bernoulli effect of the upper
surface of the wing. In fact, most of the lift is provided by Newton, pushing
on the bottom surface of the wing (With enough power, you can fly a barn
door). This speaks very loudly about the "expertise" of some of our most
prolific posters, right?

Jay in Dallas
"kmccune" <kmccune(at)somtel.net> wrote:

>--> Zenith-List message posted by: "kmccune" <kmccune(at)somtel.net>
>
>I have heard of others doing this, one I believe to be quite knowledgeable
. But I just can not see how you can get any lift from this. There is no
bottom of the airfoil.
>
>--------
>Kevin
>N701DZ Reserved
>
>
>Read this topic online here:
>
>http://forums.matronics.com/viewtopic.php?p=160531#160531
>

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PostPosted: Sat Jan 26, 2008 9:04 am    Post subject: Cabin airfoil Reply with quote

Okay, for sake of argument, we'll agree to disagree on
the relationship between the CH-701 and the Savannah.
Third hand knowledge (take it for what it's worth)is
that the Savannah boys in Alberta have commented that
the Land Africa is a rip off of the Savannah.
Doug MacDonald
CH-701 Scratch builder
NW Ontario, Canada

Do not archive

--- LRM <lrm(at)skyhawg.com> wrote:

Quote:

<lrm(at)skyhawg.com>

One thing not mentioned is the increased headroom
for those who might need
or want it. The other is the using of the term "rip
off". I remind every
one that the 701 is in fact a copy of a multitude of
parts used by
previously like aircraft, by no means is it an
original design. I would
never say it's a rip off, it's just smart
engineering of proven concepts and
parts, as is the Savanna.

LRM, skyhawg.com.


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PostPosted: Sat Jan 26, 2008 9:13 am    Post subject: Cabin airfoil Reply with quote

Hi, all,

You would lose some (maybe "a little") control authority from the
tailfeathers due to blanking of some of the prop's discharge air.

Just a thought.

Jim
CH-801
DeltaHawk diesel
Augusta GA USA


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kmccune



Joined: 22 Sep 2007
Posts: 577
Location: Wisconsin, USA

PostPosted: Sat Jan 26, 2008 11:11 am    Post subject: Re: Cabin airfoil Reply with quote

Its funny , but I am having a hard time figuring out who agrees with whom! Very Happy

Do not archive


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ronlee



Joined: 25 Dec 2006
Posts: 141

PostPosted: Sat Jan 26, 2008 12:34 pm    Post subject: Re: Cabin airfoil Reply with quote

I can assure you all that the 701 lexan roof is creating lift just as it is. When on the ground the top of the lexan window is very tight to the cross brace. I have to push very hard to create any gap. When in flight I can almost get my fingers between the cross brace and the lexan. What I don't know is if it would create more lift if it was a filled in airfoil conforming to the top of the wing. Because the windshield actually blends into the top lexan, it is in a crude way creating an airfoil.

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PostPosted: Sat Jan 26, 2008 1:25 pm    Post subject: Cabin airfoil Reply with quote

Jaybannist(at)cs.com wrote:
Quote:
In fact, most of the lift is provided by Newton, pushing on the bottom surface of the wing (With enough power, you can fly a barn door). This speaks very loudly about the "expertise" of some of our most prolific posters, right?
Louder than you think Smile


The real expert aerodynamicists out there have explained that the
circulation flow pattern around the airfoil, and the amount of air being
displaced downward, contributes far more than the Bernoulli effect or
the "planing" effect you mention. I am not an expert on the circulation
theory but I am aware that all of the real, employed, expert level
aerodynamics people 100% believe in it.


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PostPosted: Sat Jan 26, 2008 1:47 pm    Post subject: Cabin airfoil Reply with quote

Larry, I'd be interested to know what design or designs the 701 is a
copy of.Using this logic you could say that the P-51 or the Stealth
fighter is an amalgam of previously designed parts.

LRM wrote:
Quote:
I remind every one that the 701 is in fact a copy of a multitude of
parts used by previously like aircraft, by no means is it an original
design.


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