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Pitot Static Ports

 
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Paul A. Franz, P.E.



Joined: 02 Dec 2008
Posts: 280
Location: Bellevue WA

PostPosted: Tue Feb 09, 2010 5:31 am    Post subject: Pitot Static Ports Reply with quote

On Tue, February 9, 2010 2:55 am, Mark Napier (napierm) wrote:
Quote:


<http://www.scandinavian-kitfoxes.se/technical/kitfox-doc/Static-system.pdf>

Time: 04:12:30 PM PST US
Subject: Re: Kitfox-List Digest: Static port location
From: "WurlyBird" <james.t.trizzino(at)us.army.mil>

So why not just post it right here?

If you're like me and read the frequent problems with the above Skystar designed
static port mostly because of location, why not use a well designed static port. But
first, before I show you a couple, have a look at how these thing work.

<http://en.wikipedia.org/wiki/Pitot_tube>

The sensors are made as either static only, total pressure only or combined static and
total pressure. From what I see in the above Kitfox instructions is they use a total
pressure sensor in the left wing and a dual port static sensor in the rear part of the
fuselage. If you are satisfied with the total pressure sensor then you might want to
get a fabricated static sensor such as Type PS shown here:

<http://www.unitedsensorcorp.com/pitot.html>

I am going to use a combined static and total pressure sensor more like the Type PA
shown in the above URL. The discussion of errors is worth reading and understanding so
you are aware of error produced by pitch and yaw, especially.

Here are some useful discussion items related to the errors in measurement due to
where the static sensor holes are placed in the tube.

<http://www.flowkinetics.com/measurement.htm>

Given this information, maybe this will contribute to building a better mousetrap, so
to speak. At least your understanding level of the sensig problem should be improved.

As you can see, due to especially boundary layer effects, the SS design falls short.
However it probably can be lauded for simplicity and low drag.
--
Paul A. Franz
Registration/Aircraft - N14UW/Merlin GT
Engine/Prop - Rotax 914/NSI CAP
Bellevue WA

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Paul A. Franz, P.E.
Registration/Aircraft - N14UW/Merlin GT
Engine/Prop - Rotax 914/NSI CAP
Bellevue WA
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Float Flyr



Joined: 19 Jul 2006
Posts: 2704
Location: Campbellton, Newfoundland

PostPosted: Tue Feb 09, 2010 2:33 pm    Post subject: Pitot Static Ports Reply with quote

Many other aircraft use the static port on the side of the fuselage. There
was even a jet in south America that crashed because the static ports, which
are also connected to the altimeter and VSI, were covered with tape for
painting on the pilot side. As both systems in the jet were separate there
was a discontinuity between the pilot and co-pilot instruments... They
stalled in the dark. Oh yes on a jet the same probes are used it's just
they are connected to a flight computer that drives the panel instruments.

Noel


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Kitfox III-A
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WurlyBird



Joined: 16 May 2008
Posts: 207
Location: North Pole, Alaska

PostPosted: Wed Feb 10, 2010 6:51 pm    Post subject: Re: Pitot Static Ports Reply with quote

If ANYONE, EVER, crashed a Kitfox or similar aircraft due to an instrument failure they probably needed to be removed from the aviation gene pool anyway. The only instruments I rely on are the RPM and TGT. Every other instrument in the aircraft is only used to reinforce what the pilot should have already felt.

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James
Kitfox 3 / 582 / 70" IVO 2 blade GA
50 hrs on the 582 swapping for HKS 700E and Avid Cowl.
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PostPosted: Thu Feb 11, 2010 3:48 am    Post subject: Pitot Static Ports Reply with quote

Interesting contribution. Would have been more useful with some meaningful
information about building a Kitfox.
Deke
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