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#21
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Bruce Hoult wrote:
But the spar does not have to deal with the extra lift on a *long* moment arm. Well not all of it anyway. Hmm ... well a deliberately non-lifting horizontal section at the tip would reduce induced drag as well. This could be done for one angle of attack, but I don't see how it could be done for the usual range a glider uses. A winglet has the same angle of attack, independent of the wing. -- ----- Replace "SPAM" with "charter" to email me directly Eric Greenwell Washington State USA |
#22
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At 07:54 29 November 2003, Bruce Hoult wrote:
In article , Eric Greenwell wrote: Winglets reduce induced drag by effectively making the wingspan longer. Perhaps in the past, but maybe not anymo from page 104 of the Fundamentals of Sailplane Design... 'Subsequently, it has been shown that good results may be obtained with relatively small winglets. In contrast to early winglets, which were essentially upward wing extensions, recent winglet designs are optimized to diffuse the vortex rollup at the wingtip, thus reducing its strength. There is also evidence that the velocity field induced by the winglets can improve airfoil aerodynamics in the vicinity of the wing tip by prolonging laminar flow and delaying separation.' But the question is, would similar-shaped horizontal extensions to the wing have the same effect? What about multiple small span 'winglets' off the end of the wing? Birds do that. The modern winglets look a lot like a single tip-feather. -- Bruce Oh, Golly-gee! In one hundred years we've gone from bi-planes to bi-winglets! |
#23
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In my country, our gliders move forward because the wing produces thrust, and our sailboats move over the water because the sail produces thrust. Whether we should rule the world is causing much controversy. PLEASE....Readers of the World! This is not in our textbooks! Did someone in the USA write the above??? Wings produce Lift!! A by product of lift is drag! Winglets do also produce lift, and therefore drag. Possibly less than the wing? But you canot call it thrust!....... This sounds like I am in the middle of some ski instructors! Skiing is great in Aspen! Think Snow! The Redtail Hawk |
#24
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From: Paul Repacholi Date: Sat, 29 Nov 2003 18:49:16 +0800 Bruce Hoult writes: If it wasn't for class rules limiting wingspan I don't think anyone would have winglets. I wonder what class rules the 744 design has in mind Those rules which limit gate space at airport terminals. -- Jack "Heavier-than-air flying machines are impossible." -- Lord Kelvin, President, Royal Society, 1895 |
#25
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"Bob Salvo" wrote in message
... Anyone? Bob Do winglets produce thrust? (CAN winglets produce thrust?) All non-believers should read the NACA report by Whitcome, the inventor of winglets. Winglets are an airfoil and therefore produce lift. If the cord of the winglet is oriented properly, the lift vector will be angled slightly forward, hence the use of the term "thrust". Since the angle of attack of the winglet is influenced by the lift coefficient of the main wing, a significant amount of "thrust" is only produced at a very narrow range of angle of attack (aircraft speed). A significant amount of "thrust" is defined as when the forward component of lift of the winglet is greater than the drag of the winglet. Since sailplanes are flying at either a slow speed of near stall or very fast speed, the concept would not seem to be of much use for sailplanes. The winglets used on sailplanes seem to use an airfoil which has a large low drag bucket and are designed more to diminish wing tip vortices. This results in lower sailplane drag, sometimes better aileron control, and perhaps at some angle of attack of the main wing some "thrust". Duane |
#26
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soarski wrote:
In my country, our gliders move forward because the wing produces thrust, and our sailboats move over the water because the sail produces thrust. Whether we should rule the world is causing much controversy. PLEASE....Readers of the World! This is not in our textbooks! Did someone in the USA write the above??? Wings produce Lift!! A by product of lift is drag! Winglets do also produce lift, and therefore drag. Possibly less than the wing? But you canot call it thrust!....... "Thrust", for the winglet question and my remarks about gliders and sailboats, was used to mean "force in the direction of motion". Apparently, that was an unusual use of the word for some people. Here's an expanded expanation: Gravity is pulling straight down, and so can not propel the glider forward; drag is pulling the glider back, and so can not propel the glider forward. So, what is left to counteract the drag? Lift, produced by the wings. This forward force comes from the lift, which is not vertical, but tipped forward a bit. Look at any diagram showing the forces on a glider, and you will see how the lift, drag, and gravity forces accomplish this. It is not common to call this force moving the glider forward (without it, drag would bring it to stop) "thrust", but the word is sometimes used that way. I still can't answer the original question about the winglets, though. -- ----- Replace "SPAM" with "charter" to email me directly Eric Greenwell Washington State USA |
#27
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If winglets produce thrust, at what angle of attack does its thrust/drag ratio
maximise? Bob |
#28
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With the production of levity such as this, winglets are certainly
adding (a) lift to dead of winter soaring in the northern hemisphere - whether it's literally or figuratively! Bravo. |
#29
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Now, I'm confused! An airfoil cannot produce thrust
-- only 'lift.' But if an airfoil has a reverse counterpart, the two are joined at the center and rotated about an axis in a vertical plane, they are then a propeller; this produces 'thrust.' But if their pitch is differentially variable and they rotate in a horizontal plane, they are then helicopter blades; they produce 'lift.' Why don't we just combine the two words in one concept and call it 'thrift?' At 20:36 29 November 2003, Bob Salvo wrote: If winglets produce thrust, at what angle of attack does its thrust/drag ratio maximise? Bob |
#30
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Being a bit of a pedant, I have been trying to find whether the technical
definition of 'thrust' fits here, as my aerodynamics is more than a bit rusty. I cannot find any book on unpowered flight which shows more than three forces - lift; drag; weight, and might at best resolve these horizontally and vertically to label the 'horizontal component of lift'. Looking at general definitions, I would think that the backward force on the air below the wings could be defined as thrust, but the notional forward reactive force on the aircraft resulting from this couldn't! 8-) Keith "Nyal Williams" wrote in message ... Now, I'm confused! An airfoil cannot produce thrust -- only 'lift.' But if an airfoil has a reverse counterpart, the two are joined at the center and rotated about an axis in a vertical plane, they are then a propeller; this produces 'thrust.' But if their pitch is differentially variable and they rotate in a horizontal plane, they are then helicopter blades; they produce 'lift.' Why don't we just combine the two words in one concept and call it 'thrift?' At 20:36 29 November 2003, Bob Salvo wrote: If winglets produce thrust, at what angle of attack does its thrust/drag ratio maximise? Bob |
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