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#1
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Eric,
I just wanted to point out that Newton and Bernoulli based explanations for lift exist. I did reread the articles and as you note neither discusses top/bottom air pressure in any relative/absolute magnitudes. KK |
#2
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http://www.hsa.lr.tudelft.nl/~frits/fig8.jpg
Highly dependant of angle of attack (incidence?), but during cruise (5 degrees) typically only a fraction of the force is generated by the lower side of the airfoil. |
#3
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![]() Eric Greenwell wrote: Ken Kochanski (KK) wrote: "The rest is generated by lower pressure on the upper side." hmmmm ... http://www.eskimo.com/%7Ebillb/wing/airfoil.html http://www.aa.washington.edu/faculty/eberhardt/lift.htm Can you point out where these articles compare the pressures on the top and bottom surface, or some reference that gives the relative magnitudes? I was unable to find it. -- Change "netto" to "net" to email me directly Eric Greenwell Washington State USA |
#4
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True.
But I`m teaching aerodynamics in my club and it is extremely hard to explain this to people. I don`t want to confuse people with vorticity fields so the explanation "pushing air down will result in an underpressure on top and an overpressure on the lower side of the wing; that`s lift" seems to be sufficient for the understanding of lift as far as gliding is concerned. http://www.navier-stokes.net/ Not too smart to post when you`re just woken up. For those who wanna know why, just take a look at my last post ;-) Jarno Nieuwenhuize. The Netherlands |
#5
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![]() Ken Kochanski (KK) schreef: "The rest is generated by lower pressure on the upper side." hmmmm ... http://www.eskimo.com/%7Ebillb/wing/airfoil.html http://www.aa.washington.edu/faculty/eberhardt/lift.htm Erik Braun wrote: Hi Wayne, yet the majority (?) of our lift is generated from the HIGH pressure BELOW the wing. No, it only generates 1/3 of the lift. The rest is generated by lower pressure on the upper side. I recommend you read http://www.soaridaho.com/Schreder/Te...lets/Masak.htm which explains the design and function of winglets. Greetings, Erik. True. But I`m teaching aerodynamics in my club and it is extremely hard to explain this to people. I don`t want to confuse people with vorticity fields so the explanation "pushing air down will result in an underpressure on top and an overpressure on the lower side of the wing; that`s lift" seems to be sufficient for the understanding of lift as far as gliding is concerned. http://www.navier-stokes.net/ Not too smart to post when you`re just woken up. For those who wanna know why, just take a look at my last post ;-) Jarno Nieuwenhuize. The Netherlands |
#6
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True.
But I`m teaching aerodynamics in my club and it is extremely hard to explain this to people. I don`t want to confuse people with vorticity fields so the explanation "pushing air down will result in an underpressure on top and an overpressure on the lower side of the wing; that`s lift" seems to be sufficient for the understanding of lift as far as gliding is concerned. http://www.navier-stokes.net/ Not too smart to post when you`re just woken up. For those who wanna know why, just take a look at my last post ;-) Jarno Nieuwenhuize. The Netherlands |
#7
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True.
But I`m teaching aerodynamics in my club and it is extremely hard to explain this to people. I don`t want to confuse people with vorticity fields so the explanation "pushing air down will result in an underpressure on top and an overpressure on the lower side of the wing; that`s lift" seems to be sufficient for the understanding of lift as far as gliding is concerned. http://www.navier-stokes.net/ Not too smart to post when you`re just woken up. For those who wanna know why, just take a look at my last post ;-) Jarno Nieuwenhuize. The Netherlands |
#8
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True.
But I`m teaching aerodynamics in my club and it is extremely hard to explain this to people. I don`t want to confuse people with vorticity fields so the explanation "pushing air down will result in an underpressure on top and an overpressure on the lower side of the wing; that`s lift" seems to be sufficient for the understanding of lift as far as gliding is concerned. http://www.navier-stokes.net/ Not too smart to post when you`re just woken up. For those who wanna know why, just take a look at my last post ;-) Jarno Nieuwenhuize. The Netherlands |
#9
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![]() Ken Kochanski (KK) schreef: "The rest is generated by lower pressure on the upper side." hmmmm ... http://www.eskimo.com/%7Ebillb/wing/airfoil.html http://www.aa.washington.edu/faculty/eberhardt/lift.htm Erik Braun wrote: Hi Wayne, yet the majority (?) of our lift is generated from the HIGH pressure BELOW the wing. No, it only generates 1/3 of the lift. The rest is generated by lower pressure on the upper side. I recommend you read http://www.soaridaho.com/Schreder/Te...lets/Masak.htm which explains the design and function of winglets. Greetings, Erik. True. But I`m teaching aerodynamics in my club and it is extremely hard to explain this to people. I don`t want to confuse people with vorticity fields so the explanation "pushing air down will result in an underpressure on top and an overpressure on the lower side of the wing; that`s lift" seems to be sufficient for the understanding of lift as far as gliding is concerned. http://www.navier-stokes.net/ Not too smart to post when you`re just woken up. For those who wanna know why, just take a look at my last post ;-) Jarno Nieuwenhuize. The Netherlands |
#10
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![]() bagmaker wrote: I also note the return of the "plate" style winglet on latest jetliners, half above, half below the wingtip, instead of a large winglet. The latest jetliners (not including Airbus) have gone to the eagle tip configuration (swept up and back slightly like Nimbus 4's), dumping the classic style winglet. The 787 and new 747 stretch have this config, I think a couple of others. Jim |
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