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tailplane balance

 
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riddon(at)sent.com
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PostPosted: Mon Jun 25, 2007 2:37 pm    Post subject: tailplane balance Reply with quote

At the expense of showing my ignorance, why is the tailplane balanced as
it is? i.e. with the pivot point well forward of the c of g which
necessitates a balancing weight. Could it not have been designed with
the pivot point at the position of the c of g so no weight would be
needed?

Richard Iddon G-RIXS
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grahamsingleton(at)btinte
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PostPosted: Mon Jun 25, 2007 3:13 pm    Post subject: tailplane balance Reply with quote

That's for aerodynamic reasons, in the early days the pivot was moved
about a bit to avoid "short period oscillation" and the present position
was perhaps the best compromise. The pivot needs to be in front of the
centre of pressure, which can move about a bit. Symetrical sections tend
not to have moving Cp but maybe it does move a bit.
Graham

Richard Iddon wrote:
Quote:


At the expense of showing my ignorance, why is the tailplane balanced as
it is? i.e. with the pivot point well forward of the c of g which
necessitates a balancing weight. Could it not have been designed with
the pivot point at the position of the c of g so no weight would be
needed?

Richard Iddon G-RIXS


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davidjoyce(at)doctors.org
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PostPosted: Tue Jun 26, 2007 12:33 am    Post subject: tailplane balance Reply with quote

Richard, It is critical that the centre of lift or pressure is on the axis
or behind it for an all moving tail plane. If it is in front then any
increase in incidence immediately produces a force trying to further
increase that incidence. Such a system is highly unstable and would try to
snatch the stick out of your hand! If it succeeds disaster inevitably
follows.
Regards, David Joyce, G-XSDJ
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tonywickens(at)btconnect.
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PostPosted: Tue Jun 26, 2007 4:36 am    Post subject: Tailplane Balance Reply with quote

I am not moved to write often but just to add my two cents worth. Almost everything we are saying is based on supposition regarding, in particular, the tragic accident to Williams Europa. There has naturally been much speculation, particularly after the early mention of flutter as a possible cause. As with all accidents there were probably a number of mutually divergent occurancies which led to the eventual loss of control but I am waiting for the AAIB to give their findings as it would appear that a preliminary report is imminent.
<?xml:namespace prefix = o ns = "urn:schemas-microsoft-com:office:office" />
Making reference to comments in recent e-mails

If the tailplane balance weights were placed in the leading edge of each tailplane you would end up with about four times the weight of the present TP19’s (200mm arm as opposed to the 800mm at present). I don’t have access to the TP19’s at the moment but they are heavy and four times heavy is very heavy, and this would obviously be undesirable in weight and C of G terms. However it is probably correct that the mono is slightly more prone to shock loading at the pin securing the TP12. Although the ‘system’ is balanced, the tailplane is itself tail heavy, and on landing and over rough ground this couple is resisted mainly by the TP12 pins. A similar situation occurs of course with the balance weight arm at TP9 and its two pins TP14C. Pronounced pitching on the close coupled Trike gear on a rough surface would cause similar forces. Taxi-ing at slower speeds is desireable for this and many other reasons.

All design is a compromise but obviously if the balance weights were in the leading edge of the tailplane then it would avoid the above situation and each tailplane would be individually balanced as the ailerons are on the Europa. I suspect that in the original design this option was discarded in the interests of weight saving, and bearing in mind the arm length, from a weight and balance point of view.

I think there is a lot of truth in what you are hinting at. Us trigear
jockeys are having to pay dearly for shortcomings in the mono.


I don’t think comments such as those above are very helpful. All design is a compromise and the Europa was designed around a unique set of operational objectives which is why so many of us bought Europa kits. It is different to other taildraggers and requires slight modifications to standard taildragger technique as does the Pitts Special and some other more demanding aircraft. It is the only kit to have multi configuration which allows people to make a personal choice depending on their preferences. As I said at the beginning lets wait for the results of the investigation before jumping to dubious judgments.

Tony
[quote][b]


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DuaneFamly(at)aol.com
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PostPosted: Tue Jun 26, 2007 7:59 am    Post subject: Tailplane Balance Reply with quote

In a message dated 6/26/2007 5:37:08 A.M. Pacific Daylight Time, tonywickens(at)btconnect.com writes:
Quote:
It is different to other taildraggers and requires slight modifications to standard taildragger technique as does the Pitts Special and some other more demanding aircraft.


Good Day Tony,

If you have specific knowledge with regard to the Europa I would appreciate it if you could elaborate on this sentence. I have flown only Citabrias for my tailwheel transition and am building my Europa with a conventional setup. I was just wondering what adjustments I might have to make.

Thanks in advance.

Mike Duane A207A
Redding, California
XS Conventional Gear
Jabiru 3300
Sensenich R64Z N
Ground Adjustable Prop

See what's free at AOL.com.
[quote][b]


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tonywickens(at)btconnect.
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PostPosted: Tue Jun 26, 2007 11:39 am    Post subject: Tailplane Balance Reply with quote

Hi Mike
I was only referring to the Pitts as an aircraft that required just a little more training for anyone new to the type as does the Europa. I am personally not familiar with the Citabria although from what I have read that experience will be more than adequate. In the UK the PFA instituted a coaching scheme where experienced pilots are cleared to give conversion training on specific aircraft. This has worked well over here and I believe is very popular with the insurance companies. In fact I think they make such training a condition of cover. I am still building but also have a share in a monowheel and had conversion training as mentioned above. The airplane is a delight to fly but a bit more demanding on landing. I found the most difficult thing to get used to was the power and sensitivity of the elevator after other taildragers that I have flown. Having said that it is not difficult to get used to and of course it is vital to use the rudder to keep straight until the aircraft stops as is the case with all taildraggers. Hard runways are a little more testing than grass in terms of keeping straight but again this is not too demanding. I agree with the people who wisely advise to limit the cross winds building up your personal limits gradually, particularly on hard runways. Take offs are easy, holding the tail on the ground until aerodynamic aileron control is established. It is IMNSHO the best handling kit aircraft and a delight to fly and tour in. Like all aircraft types one needs to fully understand them, and as the late Tommy Sopwith so aptly put it "make friends with them". Best advice I would give is find a good coach or instructor but one experienced on the Europa and spend a few hours, four or five is not too many, until you feel comfortable with the aircraft and then very slowly expand your own envelope. The level of coach over here is very high, in fact the person that converted me was a Royal Air Force test pilot and is now a test pilot with Airbus, although they come from all backgrounds and I am sure there are many such people in California. I would think Kim Prout would be an excellent source of knowledge although California is very big and he may not live close to you. I should add that I am not a professional pilot, I am a professional engineer, now retired but I have been flying taildraggers mainly since 1959 with a beak of about 20 years when I couldn't afford to rent airplanes. So if I can fly the Europa I am sure anyone can.
Regards
Tony
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