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U2U2U2
Joined: 06 Jul 2001 Posts: 5467 Location: Shipsterns Bluff, Tasmania. Colorado
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dvCali
Joined: 23 Aug 2007 Posts: 1314
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Posted: Thu Feb 13, 2020 11:33 am Post subject: Re: Airplane lift fly wing fin |
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U2U2U2 wrote: | https://www.scientificamerican.com/article/no-one-can-explain-why-planes-stay-in-the-air/?utm_source=pocket-newtab
To those that like to compare aircraft wings to fins.
Many references when comparing a fin to wing are made to Daniel Bernoulli, who is mentioned in the link.
FWIW Bernoulli died 1782, Wright Brothers first flight 1903. |
Great article! A good example that shows how understanding even a purely physical system is very much complicated!!!!!! |
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grantmac017
Joined: 04 Aug 2016 Posts: 946
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Posted: Thu Feb 13, 2020 7:15 pm Post subject: |
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Bernoulli has much to do with carburetors, but nothing to do with wings or fins since they aren't a closed system. |
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Brian_S
Joined: 11 Jun 2005 Posts: 249 Location: SE Michigan
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Posted: Thu Feb 13, 2020 8:01 pm Post subject: |
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In an attempt to cure everyone's insomnia, I'll try to explain why I think this article was very misleading.
The equations governing flow of a continuous medium are two: Conservation of Mass, and Conservation of Momentum (a.k.a. the momemtum equation). The momentum equation does include all the physical forces that affect the pressure distribution, and thus lift, on a wing or a fin. You might think of Newton's 2nd Law as a simplification of the momentum equation.
The author did state that there was no disagreement on the equations. However, he then goes into this argument about whether it's Bernoulli's equation or Newton's law which governs the lift on a airfoil. This is where it just adds to the confusion.
The momentum equation is necessarily applied to a region of interest, often called a 'control volume' (CV). It states that the sum of all forces acting on the CV must equal to time rate change of momentum within the CV, plus the net momentum flow out of the CV. If you were to apply the momentum equation to a small region of interest, like a particle with no flow through it, then it would look like the familiar F = Ma that you've seen in physics class - Newton's Law.
(Is anyone still reading?)
If instead you apply the momentum equation to flow along a streamline, in a steady, incompressible flow field, and you neglect viscous effects and interruptions to the streamline, then you have the Bernoulli Equation. So the Bernoulli Equation is just a highly simplified version of the momentum equation.
So, it's not like Newton's laws and the Bernoulli Equation are two different theories - they are simplifications (maybe extreme simplifications, neglecting different aspects) of the same governing principle.
The article made for good reading, but instead of explaining why only a piece of the theory doesn't explain the whole phenomena, he tried to pit two pieces of the same theory against one another - which we've seen in this forum and elsewhere.
(Insert snoring sound.) _________________ Brian S
www.miwindsurfing.com
Last edited by Brian_S on Fri Feb 14, 2020 6:00 pm; edited 2 times in total |
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Brian_S
Joined: 11 Jun 2005 Posts: 249 Location: SE Michigan
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Posted: Thu Feb 13, 2020 8:02 pm Post subject: |
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grantmac017 wrote: | Bernoulli has much to do with carburetors, but nothing to do with wings or fins since they aren't a closed system. |
Bernoulli's Equation does not apply to a closed system. However, it is the most used and most abused equation in fluid mechanics. _________________ Brian S
www.miwindsurfing.com |
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U2U2U2
Joined: 06 Jul 2001 Posts: 5467 Location: Shipsterns Bluff, Tasmania. Colorado
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cgoudie1
Joined: 10 Apr 2006 Posts: 2599 Location: Killer Sturgeon Cove
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Posted: Thu Feb 13, 2020 8:04 pm Post subject: |
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I would have to disagree. Bernoulli has a lot to do with wings and fins, and propellers, and a host of other physical properties that are developed
as a result of pressure differential from difference in travel distance
in a substance. He's definitely why airplanes fly.
-Craig
grantmac017 wrote: | Bernoulli has much to do with carburetors, but nothing to do with wings or fins since they aren't a closed system. |
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boardsurfr
Joined: 23 Aug 2001 Posts: 1266
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Posted: Fri Feb 14, 2020 10:19 am Post subject: |
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Thanks, Brian, great explanation!
Brian_S wrote: | In and attempt to cure everyone's insomnia, I'll try to explain why I think this article was very misleading.
The equations governing flow of a continuous medium are two: Conservation of Mass, and Conservation of Momentum (a.k.a. the momemtum equation). The momentum equation does include all the physical forces that affect the pressure distribution, and thus lift, on a wing or a fin. You might think of Newton's 2nd Law as a simplification of the momentum equation.
The author did state that there was no disagreement on the equations. However, he then goes into this argument about whether it's Bernoulli's equation or Newton's law which governs the lift on a airfoil. This is where it just adds to the confusion.
The momentum equation is necessarily applied to a region of interest, often called a 'control volume' (CV). It states that the sum of all forces acting on the CV must equal to time rate change of momentum within the CV, plus the net momentum flow out of the CV. If you were to apply the momentum equation to a small region of interest, like a particle with no flow through it, then it would look like the familiar F = Ma that you've seen in physics class - Newton's Law.
(Is anyone still reading?)
If instead you apply the momentum equation to flow along a streamline, in a steady, incompressible flow field, and you neglect viscous effects and interruptions to the streamline, then you have the Bernoulli Equation. So the Bernoulli Equation is just a highly simplified version of the momentum equation.
So, it's not like Newton's laws and the Bernoulli Equation are two different theories - they are simplifications (maybe extreme simplifications, neglecting different aspects) of the same governing principle.
The article made for good reading, but instead of explaining why only a piece of the theory doesn't explain the whole phenomena, he tried to pit two pieces of the same theory against one another - which we've seen in this forum and elsewhere.
(Insert snoring sound.) |
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U2U2U2
Joined: 06 Jul 2001 Posts: 5467 Location: Shipsterns Bluff, Tasmania. Colorado
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Posted: Fri Feb 14, 2020 10:39 am Post subject: |
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Snoring sound. Lol.
The link I posted was in regard to references on Windsurf Forums that our fins are likened to an aircraft wing. I have not seen any discussion , in regard to foils, which because of the horizontal actual wing , instead of verticals are a wing.Duh.
What makes a airplane stay airborne, is the same as when it takes off, when lift overcomes gravity, and thrust overcomes drag.
The air is thinner at higher altitude so more lift and thrust isn’t necessary .
Some Business jets are flying at 410,00 now to take advantage of this, and because the population there is not as heavy , so a more direct course can be flown. _________________ K4 fins
4Boards....May the fours be with you
http://www.k4fins.com/fins.html
http://4boards.co.uk/ |
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grantmac017
Joined: 04 Aug 2016 Posts: 946
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Posted: Fri Feb 14, 2020 8:39 pm Post subject: |
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Bernoulli's principal is at most a minor contributor to lift compared to the Kutta–Joukowski theorem. |
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