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| | #26 |
| Old Skool Join Date: Sep 2001
Posts: 2,044
| Well, too tired with too much on my plate to get into this too much, (and I admit I really just mostly scanned where this thread has gone without reading it carefully), but it appears to me that none of what you wrote changes the basic issue, which is the downward momentum of the air is the RESULT of lift, and not the CAUSE. Nothing you have written demonstrates that it is more than just representational of the lift force, and the wing tip vorticiies are still the culprit of induced drag, the rearward tilting of the lift force and, as you say "shoving the air forward". In the end, I come away wondering what point you are trying to make? |
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| | #27 | |
| Old Skool Join Date: Sep 2003
Posts: 1,853
| Quote:
Realms, What you are saying is that this is accurate, since the wing is imparting a downward net momentum. Is my understanding correct? | |
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| | #28 |
| Old Skool Join Date: Sep 2006 Location: Memphis, TN
Posts: 2,224
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| | #29 | |
| Old Skool Join Date: Sep 2006 Location: Memphis, TN
Posts: 2,224
| Quote:
It's true that there is no net downward momentum in the vertical plane, but there is a net change in vertical momentum, and it's a change in momentum that indicates the presence of forces. So part of the confusion on the subject appears to be referring in one instance to the values of momentum and in another instance changes in momentum. The only point about bringing up the net momentum = 0 concept is to illustrate that net downward momentum cannot be causal because it does not exist. This point only has value to the extent that anyone is arguing that it's a net downward momentum that produces lift. You have not made this argument, but I believe that others have. (Your argument is that there is a net momentum change in the downward direction, which is true.) However, this momentum change is the equal and opposite reaction of the lift force generated by the airfoil. That fact that there is a momentum change is due to the fact that the air is free to accelerate. The airfoil doesn't particularly care whether this happens or not. ![]() | |
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| | #30 | ||
| Old Skool Join Date: Sep 2006 Location: Memphis, TN
Posts: 2,224
| Quote:
Quote:
You can always calculate lift by integrating the pressure differences around the airfoil. No need to take into account anything else. Or you can calculate the momentum change of the air to deduce the force that produced it. Last edited by tgrayson; November 7th, 2006 at 10:56. | ||
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| | #31 |
| Old Skool Join Date: Sep 2006 Location: Memphis, TN
Posts: 2,224
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| | #32 |
| Old Skool Join Date: Sep 2003
Posts: 1,853
| So to conclude my intial inquiry from "Understanding Flight", the downwash plays no part in lift production...but the magnitude of the momentum change is indicative of the lifting force...not causitive. |
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| | #33 | |
| Old Skool Join Date: Sep 2006 Location: Memphis, TN
Posts: 2,224
| Quote:
That's my position (at present), with the caveat that "downwash" isn't the downward momentum we're talking about. Downwash, by definition, is the extra downward momentum produced by wingtip vortices. Our discussion so far is in 2-D flow, so the downward momentum is due solely to the lift force. Give Realms a chance to respond before forming your conclusions, though. We're still not communicating on one issue and I don't want to speak for him. | |
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| | #34 |
| Old Skool Join Date: Sep 2001
Posts: 2,044
| B767, my post was meant for Realms, not you, but I withdraw it with apologies, as I missed some of what you wrote. Tgrayson, thanks, I missed some of what you quoted in my quick read, or it didn't register. Sorry for any confusion. |
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| | #35 |
| Old Skool Join Date: Sep 2003
Posts: 1,853
| No prob...I understood your context was to him. Although, fascinated, I'm just hanging on by a thread in this discussion and it was good to reiterate what it is we're trying to figure out. |
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| | #36 | |
| Junior Member Join Date: Aug 2002
Posts: 212
| Quote:
I was not aware that anyone tried to make the argument, because to me it is nonsensical. In my head I probably translated "net downward momentum" into "net change in downward momentum" as I was reading because that's the only thing that makes sense to me when talking about forces (which is the very point tgrayson was making). This led to concern that tgrayson was saying there was no change in momentum in the 2-D case (tgrayson wasn't), so I set out to show, in detail, that there was in fact a change in momentum. However, we really agreed all along. Tgrayson is correct, I'm correct, we're all correct. At least now our correctness is available in extreme detail. | |
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| | #37 |
| Old Skool Join Date: Sep 2003
Posts: 1,853
| Cool. So now I'll go back to my original post. Where are the "Understanding Flight" authors getting away with downwash being causal to lift production? Do they have supporters? Is there theory to support their claim? (Tgrayson & Realms just proved otherwise.) Are they just shooting from the hip because it sounds good? If they have no basis to justify their claims...then they are doing a lot of damage, IMO. |
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| | #38 |
| Junior Member Join Date: Aug 2002
Posts: 212
| I haven't read the book, and can't say I'm inclined to now! I did read their synopsis on their web page. Given the background of the authors my intuition is that they are likely trying to say what we are saying, but through simplification and sloppy terminology make an incorrect mess out of it, much like the pilot textbooks they claim to improve upon. |
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| | #39 | |
| Old Skool Join Date: Sep 2006 Location: Memphis, TN
Posts: 2,224
| Quote:
What do you know about the Coanda Effect? In the past, my Googling didn't turn up much authoritative about it. My fluid dynamics book only has one mention of it towards the end of the book. There seems to be some debate about whether it's a viscosity issue or surface tension. Perhaps those are related concepts. In aviation, I believe there is some application with boundary layer control and lift augmentation systems, but again there are only one or two references to it in all my books. John Denker, who wrote the online Aerodynamics book "See How it Flies", dismisses the Coanda Effect, but doesn't provide a whole lot of explanation as to why. He includes in his references a paper by a noted authority on the subject. I acquired a copy of the paper, but found it unenlightening. | |
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| | #40 |
| Junior Member Join Date: Aug 2002
Posts: 212
| In the three aerodynamics/fluid mechanics textbooks I have in my personal posession I do not recall ever coming across the "Coanda effect" term. I just checked their indices and it is not listed. The engineering library here probably has the answer, so I might look there when I have a substantial chunk of spare time. |
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| | #41 | |
| Old Skool Join Date: Sep 2006 Location: Memphis, TN
Posts: 2,224
| Quote:
That itself is interesting. Thank you. | |
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| | #42 | |
| Old Skool Join Date: Sep 2001
Posts: 2,044
| I share Tgraysons thoughts on this thread. There was some miscomm earlier on, but in the end, it served to clarify the issue really nicely! Thanks to all for a really great read! Now we have another thread we can point people to. Quote:
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