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Re: noise filters
Hi Dave,
I converted my dual Revmaster mag harness over to automotive wires and am using automotive plugs. I have never had any electrical noise from the system.
What sort of interferance problems
Hi Dave,
I converted my dual Revmaster mag harness over to automotive wires and am using automotive plugs. I have never had any electrical noise from the system.
What sort of interferance problems
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By
Rene Robertson <q2robertson@...>
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#25798
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noise filters
Hi all,
Anyone experience engine noise with the Revmaster auto plug conversion, and can suggest how to eliminate it? Do noise filters work? Thanks.......Dave Dugas
Hi all,
Anyone experience engine noise with the Revmaster auto plug conversion, and can suggest how to eliminate it? Do noise filters work? Thanks.......Dave Dugas
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By
Dave Dugas
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#25797
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Re: Air Flow at canard - fuselage intersection LS1
Quarky, this is the first time you have made any cents.
Ryan
TWENETY ONE GIGAWATS !!!! (slides the spectacles deeper in his
brow) .... im realy not that bad ... i have simply nothign better to
do
Quarky, this is the first time you have made any cents.
Ryan
TWENETY ONE GIGAWATS !!!! (slides the spectacles deeper in his
brow) .... im realy not that bad ... i have simply nothign better to
do
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By
Tri-Q1 <rryan@...>
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#25796
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Re: Help!
Larry Severson wrote:-
The Q bird has relatively large ailerons because of their placement
inboard. (This was done to achieve a simple method of control for the
builder). It should be clear from
Larry Severson wrote:-
The Q bird has relatively large ailerons because of their placement
inboard. (This was done to achieve a simple method of control for the
builder). It should be clear from
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By
Paul Buckley
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#25795
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Re: Carburetor
Thanks Bruce and all who responded.
Ron
Sonerai there and Q200 gettin there
Thanks Bruce and all who responded.
Ron
Sonerai there and Q200 gettin there
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By
Ron Triano <rondefly@...>
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#25794
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Re: Help!
Easier to build?
Probably, and being inboard would also mean that the wing would not have to be so stiff (to prevent twisting when aileron is applied) and therefore lighter.
Easier to build?
Probably, and being inboard would also mean that the wing would not have to be so stiff (to prevent twisting when aileron is applied) and therefore lighter.
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By
Paul Buckley
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#25792
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Re: Air Flow at canard - fuselage intersection LS1
or just people are tired of hearing my 2 cents .. lol .. ONE POINT TWENETY ONE GIGAWATS !!!! (slides the spectacles deeper in his brow) .... im realy not that bad ... i have simply nothign better to
or just people are tired of hearing my 2 cents .. lol .. ONE POINT TWENETY ONE GIGAWATS !!!! (slides the spectacles deeper in his brow) .... im realy not that bad ... i have simply nothign better to
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By
Jason Muscat <fifty101fifty@...>
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#25791
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Re: Air Flow at canard - fuselage intersection LS1
We are all sounding a bit past our use by date except maybe Jason is right
(as yet untested). I sort of remember something like P1V1=P2V2 ie PV is
constant in a given system and if the volume
We are all sounding a bit past our use by date except maybe Jason is right
(as yet untested). I sort of remember something like P1V1=P2V2 ie PV is
constant in a given system and if the volume
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By
Peter Harris <peterjfharris@...>
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#25790
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Re: Earnest and Donna back home.
Hi! Frances and Raoul home too.tuesday nite after a few stops on the way back to Fl. Great time. Tks Spud and your wife. Raoul
--- MartinErni@... wrote:
From: MartinErni@...
To:
Hi! Frances and Raoul home too.tuesday nite after a few stops on the way back to Fl. Great time. Tks Spud and your wife. Raoul
--- MartinErni@... wrote:
From: MartinErni@...
To:
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By
raoborg@...
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#25789
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Re: Air Flow at canard - fuselage intersection LS1
im sure i have to brush up on my dynamics (statics is so much easier) but isnt there a distinction between pressure, and what i think you are refuring to "in the direction of flow" velocity?
after
im sure i have to brush up on my dynamics (statics is so much easier) but isnt there a distinction between pressure, and what i think you are refuring to "in the direction of flow" velocity?
after
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By
Jason Muscat <fifty101fifty@...>
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#25788
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Re: Help!
Ah, the most parsimonious answer!!
Ah, the most parsimonious answer!!
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By
Mark A. Pearson <wlkabout@...>
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#25787
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Re: Help!
LOL ... ya, i can speak numbers just fine.. but when it comes to grammer/spelling etc ... hook on fonics done worked for me... :D
Mike Perry <dmperry1012@...> wrote: Jason:
It's a
LOL ... ya, i can speak numbers just fine.. but when it comes to grammer/spelling etc ... hook on fonics done worked for me... :D
Mike Perry <dmperry1012@...> wrote: Jason:
It's a
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By
Jason Muscat <fifty101fifty@...>
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#26033
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Re: Help!
Jason:
It's a good thing you aren't teaching spelling or philosophy! I am nearly
certain you are referring to the principle of parsimony known as "Occam's
Razor": entia non sunt multiplicanda
Jason:
It's a good thing you aren't teaching spelling or philosophy! I am nearly
certain you are referring to the principle of parsimony known as "Occam's
Razor": entia non sunt multiplicanda
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By
Mike Perry <dmperry1012@...>
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#25786
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Re: Air Flow at canard - fuselage intersection LS1
No, the increased pressure is perpendicular to the direction of flow. It is reduced in the direction of flow.
Larry Severson
Fountain Valley, CA 92708
(714) 968-9852
larry2@...
No, the increased pressure is perpendicular to the direction of flow. It is reduced in the direction of flow.
Larry Severson
Fountain Valley, CA 92708
(714) 968-9852
larry2@...
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By
Larry Severson
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#25785
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Re: Help!
This discussion actually belongs on the Qperformance list; however, I will sink deeper.
Washout (washin, or any twisting of the wing) makes the wing less effective as a lifting device, and increases
This discussion actually belongs on the Qperformance list; however, I will sink deeper.
Washout (washin, or any twisting of the wing) makes the wing less effective as a lifting device, and increases
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By
Larry Severson
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#25793
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Thank You
I would like to thank all the folks at Emporia for the card and
condolences for my cousin Gary. Your support and kindness were very
much appreciated.
So glad to get to see you all and fellowship with
I would like to thank all the folks at Emporia for the card and
condolences for my cousin Gary. Your support and kindness were very
much appreciated.
So glad to get to see you all and fellowship with
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By
Bruce Crain
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#25783
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Re: Air Flow at canard - fuselage intersection LS1
Earnest it is hard for me to grasp that the expanding airflow will increase
in pressure (but that's not your fault).
Peter
_____
From: Q-LIST@... [mailto:Q-LIST@...]
Earnest it is hard for me to grasp that the expanding airflow will increase
in pressure (but that's not your fault).
Peter
_____
From: Q-LIST@... [mailto:Q-LIST@...]
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By
Peter Harris <peterjfharris@...>
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#25782
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Re: Carburetor
Ron,
My good friend Gene Martin owns Martin Induction (FAA repair station).
He works on carbs, turbos, fuel injectors, etc. Send him and e-mail
and tell him I sent you.
<genemartin@...>
Bruce
Ron,
My good friend Gene Martin owns Martin Induction (FAA repair station).
He works on carbs, turbos, fuel injectors, etc. Send him and e-mail
and tell him I sent you.
<genemartin@...>
Bruce
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By
Bruce Crain
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#25781
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Re: Help!
great simple answer, hakim's razor (i think i speled that correctly) that makes perfect sence ...
Doug Humble <hawkidoug@...> wrote: I think the ailerons are on the inside because it
great simple answer, hakim's razor (i think i speled that correctly) that makes perfect sence ...
Doug Humble <hawkidoug@...> wrote: I think the ailerons are on the inside because it
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By
Jason Muscat <fifty101fifty@...>
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#25778
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Re: Help!
I think the ailerons are on the inside because it was easier to build that way.
Doug "Hawkeye" Humble
A Sign Above www.asignabove.net
Omaha NE
N25974
I think the ailerons are on the inside because it was easier to build that way.
Doug "Hawkeye" Humble
A Sign Above www.asignabove.net
Omaha NE
N25974
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By
Doug Humble <hawkidoug@...>
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#25776
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