Today's Message Index:
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1. 05:14 AM - Re: giblets (womenfly2)
2. 02:59 PM - Re: Re: giblets (jim hyde)
3. 07:38 PM - Re: Re: giblets (Steven Dortch)
4. 08:26 PM - Phishing attack (Ken Bickers)
5. 08:34 PM - Re: Re: giblets (jim hyde)
Message 1
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The side area of a fuselage is part of the design calculations on the yaw stability
along the vertical axis which includes the fin area. The area removed would
have to be calculated for the loss area of the fuselage sides an added to the
fin to keep the stability as designed.
Just my 2-cents worth .... WF2
--------
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=421554#421554
Message 2
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ood thanks=0Ajim=0AOn Friday, April 4, 2014 7:24 AM, womenfly2 <Love2Fly.KA
" <Love2Fly.KAP@gmail.com>=0A=0AThe side area of a fuselage is part of the
design calculations on the yaw stability along the vertical axis which incl
udes the fin area. The area removed would have to be calculated for the los
s area of the fuselage sides an added to the fin to keep the stability as d
esigned.=0A=0AJust my 2-cents worth .... WF2=0A=0A--------=0A=0A=0A=0A=0A
=0A=0ARead this topic online here:=0A=0Ahttp://forums.matronics.com/viewtop
- - - - - - - - - - - - - - - -Matt Dralle, L
=======
Message 3
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Below is a response from my buddy the aerodynamacyst. He is also a plane
ownerr of some experience. I asked him about effects of drag, slipping and
would streamlinig the exposed wood/tubes help.
G'day Steve,
Yes, the drag will be increased with an exposed fuselage structure.
Will it fly? That depends on the available thrust horsepower available.
Enough, and it will
fly.
The next question is: How does not covering the fuselage affect the
stability and control
as well as the balance of the aircraft? Unknown.
Slipping should work. The exposed fuselage may, or may not, have more drag
than the
covered fuselage in a slip.
Streamlining might help the aerodynamics but may not help the structural
strength.
If left uncovered, the owner will not just be a test pilot for a known
design, but
an EXPERIMENTAL test pilot for an "unknown" design.
Dave Rogers
On Fri, Apr 4, 2014 at 4:58 PM, jim hyde <jnl96@yahoo.com> wrote:
> ood thanks
> jim
> On Friday, April 4, 2014 7:24 AM, womenfly2 <Love2Fly.KAP@gmail.com>
> wrote:
> >
>
> The side area of a fuselage is part of the design calculations on the yaw
> stability along the vertical axis which includes the fin area. The area
> removed would have to be calculated for the loss area of the fuselage sides
> an added to the fin to keep the stability as designed.
>
> Just my 2-cents worth .... WF2
>
> --------
>
>
> Read this topic online here:
>
> http://forums.matronics.com/viewtopic.php?p=421554#421554
>
> /Navigator?Pietenpol-List" target="_blank">http://www.matronics.com/Navig
> - MATRONICS WEB FORUMS= &n-->
> http://ww======================
>
>
> <http://www.matronics.com/contribution>
>
> *
>
>
> *
>
>
--
Blue Skies,
Steve D
Message 4
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Folks,
It appears that my userid is currently being used as an alias in a phishing
attack. Please do not open any email that appears to be coming from me
that asks you to open a Google Doc file. I have not sent such an email and
apologize in advance for the inconvenience.
My best, Ken Bickers
Message 5
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thanks jim=0AOn Friday, April 4, 2014 9:48 PM, Steven Dortch <steven.d.dort
ch@gmail.com> wrote:=0A =0ABelow is a response from my buddy the aerodynam
acyst. He is also a =0Aplane ownerr of some experience. I asked him about e
ffects of drag, =0Aslipping and would streamlinig the exposed wood/tubes he
lp. =0A=0A=0A=0A=0AG'day Steve,=0A=0AYes, the drag will be increased with a
n exposed fuselage structure.=0A=0AWill it fly? That depends on the availab
le thrust horsepower available. Enough, and it will=0Afly.=0A=0AThe next qu
estion is: How does not covering the fuselage affect the stability and cont
rol=0Aas well as the balance of the aircraft? Unknown.=0A=0ASlipping should
work. The exposed fuselage may, or may not, have more drag than the=0Acove
red fuselage in a slip.=0A=0AStreamlining might help the aerodynamics but m
ay not help the structural strength.=0A=0AIf left uncovered, the owner will
not just be a test pilot for a known design, but=0Aan EXPERIMENTAL test pi
lot for an "unknown" design.=0A=0ADave Rogers=0A=0A=0A=0AOn Fri, Apr 4, 201
4 at 4:58 PM, jim hyde <jnl96@yahoo.com> wrote:=0A=0Aood thanks=0A>jim=0A>O
n Friday, April 4, 2014 7:24 AM, womenfly2 <Love2Fly.KAP@gmail.com> wrote:
mail.com>=0A>=0A>The side area of a fuselage is part of the design calculat
ions on the yaw stability along the vertical axis which includes the fin ar
ea. The area removed would have to be calculated for the loss area of the f
uselage sides an added to the fin to keep the stability as designed.=0A>=0A
>Just my 2-cents worth .... WF2=0A>=0A>--------=0A>=0A>=0A>=0A>=0A>=0A>=0A>
=0A>Read this topic online here:=0A>=0A>http://forums.matronics.com/viewtop
ic.php?p=421554#421554=0A>=0A>/Navigator?Pietenpol-List" target="_blank
">http://www.matronics.com/Navig=- - - - - - - - MATRONICS
WEB FORUMS=- - - - - - - - - - &n--> http://ww==
======================0A>=0A>=0A>
=0A>=0A>=0A> =0A>" target="_blank">http://www.matronics.com/Navigator?
Pietenpol-List=0Atp://forums.matronics.com=0A_blank">http://www.matronics.c
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