Today's Message Index:
----------------------
1. 10:20 AM - Re: Another Cruiser first. (jerzy krasinski)
2. 11:52 AM - Re: Another Cruiser first. (Alfred Rosa)
3. 12:49 PM - Re: Another Cruiser first. (Robert Reed)
Message 1
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| Subject: | Re: Another Cruiser first. |
Except, if you do nod blend it perfectly with the rest of the airfoil, for
sure it would destroy the laminar flow.That converts into loosing speed....
.
Jerzy
On Sunday, April 24, 2016 2:55 PM, Robert Reed <robertr237@att.net> wro
te:
That sounds like a lot of work but may be worth the effort if you ever enco
unter a bird strike.
Superior IOF-360.=C2-
Bob Reed
Sent from my iPhone
> On Apr 24, 2016, at 2:42 PM, Alfred Rosa <fredorosa@gmail.com> wrote:
>
>
> Got the SS online from a manufacturer of sheet steel.=C2- It was a 50'
roll of 8"cut off.=C2- A bitch to bend lengthwise even though it's thin s
tuff.=C2- Had to use two angle irons - one on each side - and squeeze tog
ether with pipe clamps. I laid a pipe on the SS to help control the shape o
f the bend.
>
> Bob, I saw pics of a Lycoming hanging off the nose of your plane on your
web site.=C2- I could have sworn you had gotten a Continental.
>
> Al
>
>
> Sent from my iPhone
>
>> On Apr 24, 2016, at 2:57 PM, Robert Reed <robertr237@att.net> wrote:
>>
>>
>> Al
>>
>> That looks good and sounds like a great way to protect the leading edges
. Where did you get the SS?
>>
>>
>> Bob Reed
>> Sent from my iPhone
>>
>>> On Apr 23, 2016, at 7:52 PM, Alfred Rosa <fredorosa@gmail.com> wrote:
>>>
>>> OC,=C2- Here's the stainless leading edges on the tail feathers.
>>> The wings will have the same.
>>>
>>> I decided to do this because I wanted a different look from the usual w
hite plane with wavy colored lines.
>>>
>>> The useful attribute is protection from dings by kicked up pebbles, etc
.
>>>
>>> Al
>>> <IMG_0621.jpg>
>>
>>
>>
>>
>>
>>
>
>
>
>
>
S -
WIKI -
-
=C2- =C2- =C2- =C2- =C2- -Matt Dralle, List Admin.
Message 2
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| Subject: | Re: Another Cruiser first. |
Perfect laminar flow does not exist in nature or aircraft .
On Tue, Apr 26, 2016 at 1:20 PM, jerzy krasinski <
jerzy_krasinski@sbcglobal.net> wrote:
> Except, if you do nod blend it perfectly with the rest of the airfoil, for
> sure it would destroy the laminar flow.
> That converts into loosing speed.....
>
> Jerzy
>
>
> On Sunday, April 24, 2016 2:55 PM, Robert Reed <robertr237@att.net> wrote:
>
>
>
> That sounds like a lot of work but may be worth the effort if you ever
> encounter a bird strike.
>
> Superior IOF-360.
>
> Bob Reed
> Sent from my iPhone
>
> > On Apr 24, 2016, at 2:42 PM, Alfred Rosa <fredorosa@gmail.com> wrote:
> >
> >
> > Got the SS online from a manufacturer of sheet steel. It was a 50' roll
> of 8"cut off. A bitch to bend lengthwise even though it's thin stuff. Had
> to use two angle irons - one on each side - and squeeze together with pipe
> clamps. I laid a pipe on the SS to help control the shape of the bend.
> >
> > Bob, I saw pics of a Lycoming hanging off the nose of your plane on your
> web site. I could have sworn you had gotten a Continental.
> >
> > Al
> >
> >
> > Sent from my iPhone
> >
> >> On Apr 24, 2016, at 2:57 PM, Robert Reed <robertr237@att.net> wrote:
> >>
> >>
> >> Al
> >>
> >> That looks good and sounds like a great way to protect the leading
> edges. Where did you get the SS?
> >>
> >>
> >> Bob Reed
> >> Sent from my iPhone
> >>
> >>> On Apr 23, 2016, at 7:52 PM, Alfred Rosa <fredorosa@gmail.com> wrote:
> >>>
> >>> OC, Here's the stainless leading edges on the tail feathers.
> >>> The wings will have the same.
> >>>
> >>> I decided to do this because I wanted a different look from the usual
> white plane with wavy colored lines.
> >>>
> >>> The useful attribute is protection from dings by kicked up pebbles,
> etc.
> >>>
> >>> Al
> >>> <IMG_0621.jpg>
> >>
> >>
> >>
> >>
> >>
> tp://www.matronics.com/Navigator?KIS-List" target="_blank">
> http://www.matnbsp; t; http
>
>
> <http://www.matronics.com/contribution>
>
Message 3
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| Subject: | Re: Another Cruiser first. |
I can speak from experience that a dead on bird strike to the leading edge
of the wing does in fact destroy the laminar flow along with clean underwea
r.=C2- It totally flattened the outer most 3 feet of a Cessna 172 wing.
=C2-
Bob
From: jerzy krasinski <jerzy_krasinski@sbcglobal.net>
To: "kis-list@matronics.com" <kis-list@matronics.com>
Sent: Tuesday, April 26, 2016 12:20 PM
Subject: Re: KIS-List: Another Cruiser first.
Except, if you do nod blend it perfectly with the rest of the airfoil, for
sure it would destroy the laminar flow.That converts into loosing speed....
.
Jerzy
On Sunday, April 24, 2016 2:55 PM, Robert Reed <robertr237@att.net> wro
te:
That sounds like a lot of work but may be worth the effort if you ever enco
unter a bird strike.
Superior IOF-360.=C2-
Bob Reed
Sent from my iPhone
> On Apr 24, 2016, at 2:42 PM, Alfred Rosa <fredorosa@gmail.com> wrote:
>
>
> Got the SS online from a manufacturer of sheet steel.=C2- It was a 50'
roll of 8"cut off.=C2- A bitch to bend lengthwise even though it's thin s
tuff.=C2- Had to use two angle irons - one on each side - and squeeze tog
ether with pipe clamps. I laid a pipe on the SS to help control the shape o
f the bend.
>
> Bob, I saw pics of a Lycoming hanging off the nose of your plane on your
web site.=C2- I could have sworn you had gotten a Continental.
>
> Al
>
>
> Sent from my iPhone
>
>> On Apr 24, 2016, at 2:57 PM, Robert Reed <robertr237@att.net> wrote:
>>
>>
>> Al
>>
>> That looks good and sounds like a great way to protect the leading edges
. Where did you get the SS?
>>
>>
>> Bob Reed
>> Sent from my iPhone
>>
>>> On Apr 23, 2016, at 7:52 PM, Alfred Rosa <fredorosa@gmail.com> wrote:
>>>
>>> OC,=C2- Here's the stainless leading edges on the tail feathers.
>>> The wings will have the same.
>>>
>>> I decided to do this because I wanted a different look from the usual w
hite plane with wavy colored lines.
>>>
>>> The useful attribute is protection from dings by kicked up pebbles, etc
.
>>>
>>> Al
>>> <IMG_0621.jpg>
>>
>>
>>
>>
>>
tp://www.matronics.com/Navigator?KIS-List" target="_blank">http://www.mat
nbsp; =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2-
t; http
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