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#11
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I've seen referencs to "such and such an aircraft has a flying tail". I
imagine it means "out of the slipstream", but it sound sort of dumb to me. Is it more than marketspeak? Does "flying tail" actually mean something? Wasn't it "all-flying tail"? And didn't it refer to stabilators? I took it to mean that instead of changing the chord, as with elevators, the angle of attack of the horizontal stabilizer changed. The implication might have been that there was less drag, or less change of drag, that way. I've always heard it to mean stabilator, for pitch control, so that the the entire horizontal tail surface is "flown." This would be as opposed/compared to a fixed stabilizer and moveable elevator, which has the effect of variable camber. The same can be done with the vertical tail, although the only place I have personally seen it was a Folker Triplane replica. It flew quite well, at the hands of a very good pilot, but what I saw indicated that I was NOT qualified to try it. (Back then, planes flew much closer to people on the ground, and observers could be quite close to the runway, so the required rudder work was more visible.) Peter |
#12
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The term was originally coined by North American Aviation Company to
describe the new powered stabilator on their F86E. Prior to the E model, the Sabre had a conventional horizontal stabilizer. The E had boosted controls all around and an artificial sensing feedback into the stick that duplicated normal stick forces for the pilot. Very innovative, and the harbinger of things that came after. Made it much easier to control the 86 in pitch as the shock wave going through the transonic region passed the stabilizer. No elevator....no hinge to trap the shock wave....very smooth transonic transition for the 86. Your generic ole' Cherokee 140 has a flying tail........not boosted of course...unless somebody tries to lift the airplane by the tail while pushing it on the ground which is usually met by the owner of the bird with threats of bodily harm and injury :-)) Dudley Henriques "Jose" wrote in message et... In the context of aircraft said to have a "flying tail", what does "flying" mean? I mean, if the tail isn't flying, neither is the airplane, right? Jose -- He who laughs, lasts. for Email, make the obvious change in the address. |
#13
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Peter Dohm wrote:
the effect of variable camber. The same can be done with the vertical tail, although the only place I have personally seen it was a Folker Triplane replica. It flew quite well, at the hands of a very good pilot, but what I saw indicated that I was NOT qualified to try it. (Back then, planes flew much closer to people on the ground, and observers could be quite close to the runway, so the required rudder work was more visible.) Peter The 601XL I'm building has an all flying vertical tail. www.peoamerica.net/N601WR |
#14
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Jose wrote:
Troll or real? Real. I've seen referencs to "such and such an aircraft has a flying tail". I imagine it means "out of the slipstream", but it sound sort of dumb to me. Is it more than marketspeak? Does "flying tail" actually mean something? They are also called stabilators (at least I think that is Piper's nomenclature for the PA28 family). The entire horizontal tail moves when youy move the controls vs. just the elevator on a traditional horizontal tail. So, you are "flying" or controlling the entire horizontal tail surface. I'm not sure what the aerodynamic pros can cons are, but having flown well over 100 hours in Pipers and much more in Cessnas, I haven't seen a huge difference. The biggest difference I've seen in the Arrow I fly now as that almost as soon as it touches down you lose a fair bit of elevator authority and it tends to drop the nosewheel a little more harshly than I prefer. None of the Cessnas I've flow had the tendency. The nose would gradually drop with airspeed during the roll-out. Matt |
#15
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Typically refers to one of these: http://en.wikipedia.org/wiki/Stabilator
-- Geoff The Sea Hawk at Wow Way d0t Com remove spaces and make the obvious substitutions to reply by mail When immigration is outlawed, only outlaws will immigrate. "Jose" wrote in message et... In the context of aircraft said to have a "flying tail", what does "flying" mean? I mean, if the tail isn't flying, neither is the airplane, right? Jose -- He who laughs, lasts. for Email, make the obvious change in the address. |
#16
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So, you are "flying" or controlling the entire horizontal tail surface.
Ok, that's my first hint at the meaning of "flying" in that context. Controlling. Jose -- He who laughs, lasts. for Email, make the obvious change in the address. |
#17
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The same can be done with the vertical tail, although the only place
I have personally seen it was a Folker Triplane replica. It flew quite well, at the hands of a very good pilot, but what I saw indicated that I was NOT qualified to try it. (Back then, planes flew much closer to people on the ground, and observers could be quite close to the runway, so the required rudder work was more visible.) The 601XL I'm building has an all flying vertical tail. www.peoamerica.net/N601WR Darn! I swear I saw pictures of that--and forgot. Peter |
#18
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I'm not sure what the aerodynamic pros can cons are, but having flown
well over 100 hours in Pipers and much more in Cessnas, I haven't seen a huge difference. The biggest difference I've seen in the Arrow I fly now as that almost as soon as it touches down you lose a fair bit of elevator authority and it tends to drop the nosewheel a little more harshly than I prefer. None of the Cessnas I've flow had the tendency. The nose would gradually drop with airspeed during the roll-out. I suspect, but don't really know, that the placement of the main undercarriage is a greater factor in the effect than the stabilator. I vaguely recall that Piper took advantage of the greater control authority possible with the stabilator to install a slightly smaller horizontal tail surface on one or more models--although I thought that it was the Archer. The PA-38 Tomahawk, which had a Tee mounted fixed stabilizer and moveable elevator, exhibited essentially the same trait. If you held the nose off, it would drop rather precipitously. It also had the main undercarriage mounted farther aft than a Cessna of similar weight--presumably to prevent tipping the aircraft on its tail when the boarding step was in use. The high wing Cessnas faced no such consideration, and the nose wheel could be held off much longer and dropped more slowly. Peter |
#19
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In article ,
"Peter Dohm" wrote: I'm not sure what the aerodynamic pros can cons are, but having flown well over 100 hours in Pipers and much more in Cessnas, I haven't seen a huge difference. The biggest difference I've seen in the Arrow I fly now as that almost as soon as it touches down you lose a fair bit of elevator authority and it tends to drop the nosewheel a little more harshly than I prefer. None of the Cessnas I've flow had the tendency. The nose would gradually drop with airspeed during the roll-out. I suspect, but don't really know, that the placement of the main undercarriage is a greater factor in the effect than the stabilator. I vaguely recall that Piper took advantage of the greater control authority possible with the stabilator to install a slightly smaller horizontal tail surface on one or more models--although I thought that it was the Archer. fyi - Later cherokees (including the Archer) have a large stabilator than the earlier cherokees. -- Bob Noel Looking for a sig the lawyers will hate |
#20
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Peter Dohm wrote:
I'm not sure what the aerodynamic pros can cons are, but having flown well over 100 hours in Pipers and much more in Cessnas, I haven't seen a huge difference. The biggest difference I've seen in the Arrow I fly now as that almost as soon as it touches down you lose a fair bit of elevator authority and it tends to drop the nosewheel a little more harshly than I prefer. None of the Cessnas I've flow had the tendency. The nose would gradually drop with airspeed during the roll-out. I suspect, but don't really know, that the placement of the main undercarriage is a greater factor in the effect than the stabilator. I vaguely recall that Piper took advantage of the greater control authority possible with the stabilator to install a slightly smaller horizontal tail surface on one or more models--although I thought that it was the Archer. The PA-38 Tomahawk, which had a Tee mounted fixed stabilizer and moveable elevator, exhibited essentially the same trait. If you held the nose off, it would drop rather precipitously. It also had the main undercarriage mounted farther aft than a Cessna of similar weight--presumably to prevent tipping the aircraft on its tail when the boarding step was in use. The high wing Cessnas faced no such consideration, and the nose wheel could be held off much longer and dropped more slowly. Yes, I definitely can't say this is a flying tail feature, I just know that making a smooth nosewheel touchdown in the Arrow requires you to land well above stall speed. Anything within about 5 MPH of stall and the nose comes down briskly, often enough to get a slight bounce. Nothing dangerous, just annoying and makes it harder to impress the passengers! :-) Matt |
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