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#1
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There are actually 3 variants 4 if you count the fixed U/C one
they are B4 PC11 B4 PC11A B4 PC11AF Peter. Hey Peter...I missed that! I never knew there was a fixed gear version. I had a B4 for a few years and I think it was the best metal work I've ever seen. Come to think of it, I once saw a yellow one and a white one, so that makes it five ;-) Jim Vincent N483SZ illspam |
#2
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Whats your point the B4 is a T Tail, I fly one
Someone implied that aerobatic gliders don't have T tails. Rgds, Derrick Steed |
#3
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Derrick Steed wrote:
Someone implied that aerobatic gliders don't have T tails. It was me. I wrote: Any *serious* aerobatic plane ... etc. The point is, the B4 was *not* designed as an acro glider. Only later they found that due to it's superior handling it would make an ideal acro glider. The structure had to be reinforced, though, to allow flick maneuvres ... exactly because of the huge torque forces caused by the T-tail. BTW: There are many gliders which are certificated for some acro figures: ASK-21, DG-500, DG-1000 just to name a few. All of them have T-tail, none of them is primarily an acro glider, all are cross country gliders which just happen to be allowed for some simple acro figures, and, you guessed it, none of them is certificated for flick maneuvres. Stefan |
#4
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Stefan wrote:
BTW: There are many gliders which are certificated for some acro figures: ASK-21, DG-500, DG-1000 just to name a few. All of them have T-tail, none of them is primarily an acro glider, all are cross country gliders which just happen to be allowed for some simple acro figures, and, you guessed it, none of them is certificated for flick maneuvres. The flight manual for my T-tailed DG-303 Acro allowed flick maneuvers and tail slides... Marc |
#5
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Marc Ramsey wrote:
The flight manual for my T-tailed DG-303 Acro allowed flick maneuvers and tail slides... Lucky you. Lucky me that I didn't explicitely mention the DG-300. Seriously, I only wanted to say that all airplanes which are primarily designed for serious, competitive aerobatics have a "conventional" tail. All which I know, that is. (And yes, the salto has a V-tail, which isn't worse, torqueforcewise.) Of course there are many airplanes with T-tail which are allowed for aerobatics to some degree, and some might even be allowed for flick maneuvres. What was the question again? Ah, pros and cons of T-tail vs. conventional. Stefan |
#6
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Marian Aldenhövel wrote:
Hi, I have noticed that most if not all modern gliders are built with a T-Tail (not sure about the term, I am talking about the elevator being located at the top of the tailfin). While most power-aircraft I know right up to the airliners have it at the bottom. What are the aerodynamic or constructive reasons for that? Aerodynamics, Ha! It looks cool. That's what sells gliders. ;-) Shawn |
#7
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FYI: Flick half rolls are allowed in the DG-1000 (18M).
BTW: There are many gliders which are certificated for some acro figures: ASK-21, DG-500, DG-1000 just to name a few. All of them have T-tail, none of them is primarily an acro glider, all are cross country gliders which just happen to be allowed for some simple acro figures, and, you guessed it, none of them is certificated for flick maneuvres. Stefan |
#8
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Quote: " I see no significant difference in the pitch torque generated
by a T tail and a conventional tail (apart from a minimally longer arm for a T tail on a given typical glider design). "Am I missing something?" Yes. It's not pitch torque that is the issue. It is the torque on the fin/fuselage junction about the glider's longitudinal axis, caused by asymmetric and/or inertia forces of a tailplane mounted at the top of the fin - maximum moment arm. That is much greater than from a tailplane on or close to the fuselage level where its moment arm is much less. I had a share in a T-tail glider where the fin/fuselage area delaminated during a final glide with violent oscillations of the whole empennage before the pilot reduced speed and landed safely. Chris N. |
#9
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Marian Aldenhövel wrote in message ...
Hi, I have noticed that most if not all modern gliders are built with a T-Tail (not sure about the term, I am talking about the elevator being located at the top of the tailfin). While most power-aircraft I know right up to the airliners have it at the bottom. What are the aerodynamic or constructive reasons for that? Ciao, MM It's nothing to do with aesthetics. It's just a happy coincidence that aerodynamically efficient structures are beautiful things (and not just for gliders). Three reasons that may be significant are that: 1) The stabiliser is likely to be raised above the level of any crop that the pilot may land in - therefore it will not be removed by injudicious field-selection. 2) Also, I think I have read that a T-tail configuration produces one less vortex than a conventional tail arrangement:- a vortex is spawned from the end of each free tip of a tail surface (stabiliser or rudder) therefore the top of the fin will not produce a vortex in a T-tail arrangement (as the stabiliser prevents the fin from having a free tip in the air stream). A vortex causes drag, therefore a T-tail will be marginally more aerodynamically efficient. 3) Spin recovery is easier when the stabiliser is not in the turbulence of a spinning main-plane - as is more likely to be the case with a T-tail. Therefore a T-tail may be a safer aeroplane for low-time pilots. Jon. |
#10
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