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On Oct 3, 1:33 pm, wrote:
On Oct 3, 10:56 am, Le Chaud Lapin wrote: On Oct 3, 10:34 am, wrote: Both Newton and Bernoulli are correct. Even inside a pipe the static pressure drops as velocity increases. That's why your bottom table jumps as you yank off the top one: you accelerated an airflow. And in generating lift there's a displacement of air. Can't escape that at all. Also, if you don't mind, I would like to understand what you mean here. It's not clear to me. [explanation of Bernoulli's principle clipped]. I did not mean that I did not understand Bernoulli's principle. What I am saying is that I do not believe that the bottom table jumps because of airflow acceleration. In fact, if I were to use tables with circular faces, and put the entire apparatus in a giant cylindrical tube, and pull up on the top table, assuming that the very bottom of the tube were open-ended, the bottom table would follow the top table upward, no matter how fast any air inside the tube were moving. I could move the top table one molecular diameter every 10,000,000 years, and after the top table has moved, say, 0.5 meters, the bottom table will follow. This assumes, of course, that the appartus is airtight, that no air from outside the tube can squeeze in between the walls of table and tube to fill the void that was created. There are 14.7 lbs per square inch of pressure pressing upward against the underside of the bottom table. The yanking of the top table creates a vacuum between the two faces of the table. The lack of pressure on the top of the bottom table leaves nothing to counteract the pressure pressing upward on the underside of the bottom table. Then the only thing holding the bottom table on the floor is gravity. Assuming that the table is a typical table of typical weight and size, one is guranteed that the impulse net pressure of 14.7lbs / in^2 is enough to overcome gravity and lift the bottom table off the floor. Note that this really has nothing to do with Bernoulli's principle or dynamic pressures. If it is still not clear, put the assembly in a tube again, anchor the bottom table with a tie wire so it cannot move upward, and using a hydraulic jack, pull the top table upward, then stop, wait a minute, have a Coke (sipping with a straw of course), then take cutters and snap the wire holding the bottom table to the floor. At the precise moment that the wire is snapped, there is no movement of anthing at all. There is no Bernoulli action. The bottom table will rush up toward the top table, even slamming against it quite hard if the coefficient of sliding friction between table-side and tube wall is low enough. -Le Chaud Lapin- |
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On 3 Oct, 21:11, Le Chaud Lapin wrote:
On Oct 3, 1:33 pm, wrote: On Oct 3, 10:56 am, Le Chaud Lapin wrote: On Oct 3, 10:34 am, wrote: Both Newton and Bernoulli are correct. Even inside a pipe the static pressure drops as velocity increases. That's why your bottom table jumps as you yank off the top one: you accelerated an airflow. And in generating lift there's a displacement of air. Can't escape that at all. Also, if you don't mind, I would like to understand what you mean here. It's not clear to me. [explanation of Bernoulli's principle clipped]. I did not mean that I did not understand Bernoulli's principle. What I am saying is that I do not believe that the bottom table jumps because of airflow acceleration. In fact, if I were to use tables with circular faces, and put the entire apparatus in a giant cylindrical tube, and pull up on the top table, assuming that the very bottom of the tube were open-ended, the bottom table would follow the top table upward, no matter how fast any air inside the tube were moving. I could move the top table one molecular diameter every 10,000,000 years, and after the top table has moved, say, 0.5 meters, the bottom table will follow. This assumes, of course, that the appartus is airtight, that no air from outside the tube can squeeze in between the walls of table and tube to fill the void that was created. There are 14.7 lbs per square inch of pressure pressing upward against the underside of the bottom table. The yanking of the top table creates a vacuum between the two faces of the table. The lack of pressure on the top of the bottom table leaves nothing to counteract the pressure pressing upward on the underside of the bottom table. Then the only thing holding the bottom table on the floor is gravity. Assuming that the table is a typical table of typical weight and size, one is guranteed that the impulse net pressure of 14.7lbs / in^2 is enough to overcome gravity and lift the bottom table off the floor. Note that this really has nothing to do with Bernoulli's principle or dynamic pressures. If it is still not clear, put the assembly in a tube again, anchor the bottom table with a tie wire so it cannot move upward, and using a hydraulic jack, pull the top table upward, then stop, wait a minute, have a Coke (sipping with a straw of course), then take cutters and snap the wire holding the bottom table to the floor. At the precise moment that the wire is snapped, there is no movement of anthing at all. There is no Bernoulli action. The bottom table will rush up toward the top table, even slamming against it quite hard if the coefficient of sliding friction between table-side and tube wall is low enough. Whoowh! Zero point energy! In my own kitchen! I can tell the electric company to **** off now. Bertie |
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On Oct 3, 4:14 pm, Bertie the Bunyip
wrote: Whoowh! Zero point energy! Surely, you must be joking. The exposition I wrote above is nothing more than high school physics. Where do you see me implying zero point energy? I know my physics. Do you? There is no "zero point" energy. Plain and simple: If a person sucks on a straw, the reason the fluid rises has *NOTHING* to do with Bernoull's principle. It has to do with the balance in force being eliminated. In particular, the air in the straw is removed, so the 14.4lbs/square in will lift the fluid in the straw. This should be familiar to you, since you are a pilot. Where do you think 29.92 Hg comes from? It comes from the height that a column of mercury will rise in a complete rarefied tube in STP, which just happens to be 29.92. Both you and Mxmanic are wrong. -Le Chaud Lapin- |
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Le Chaud Lapin wrote:
Both you and Mxmanic are wrong. -Le Chaud Lapin- ooooo.....wait for it.....here it comes.... -- Message posted via http://www.aviationkb.com |
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On Oct 3, 4:04 pm, Le Chaud Lapin wrote:
If a person sucks on a straw, the reason the fluid rises has *NOTHING* to do with Bernoull's principle. It has to do with the balance in force being eliminated. In particular, the air in the straw is removed, so the 14.4lbs/square in will lift the fluid in the straw. So, if it has nothing to do with Bernoulli, what has it to do with lift? With tables and straws and the like we're talking static, not dynamic pressures. The airplane uses dynamic AND static pressures. In cruise flight (low AOA), I would expect a reduced pressure on the bottom of the wing, though not as low as on the top. The velocity of air across the bottom will drop its pressure, there, too. Air has mass. Anytime you try to push it out of the way, there will be some reaction. Newton says so. We know this as drag. But we also know it as lift reaction. A flat plate flying through the air at some tiny angle of attack doesn't have much faster air over the top than the bottom, if any difference at all, yet it will generate plenty of lift. Try this on, if you want to think outside the box: The airfoil we know is just that: a foil (device to deceive) to trick the air into flowing over it without breaking up at much higher angles of attack than a flat plate would let us. So the leading edge has to have some radius so the air can get around the corner from the natural stagnation point under the LE at high AOA, and that curve must gradually taper off toward the rear or the now- disturbed air would want to separate and turbulate, and if it did that it would then slow down dramatically, pressure would rise and lift would decrease. But, happily, Newton is still at work underneath so the airplane falls, but not as if the wings fell off. We're still moving forward and the wing is still shoving air out of the way downward, so lift is still generated. Dan |
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On Oct 3, 5:56 pm, wrote:
So, if it has nothing to do with Bernoulli, what has it to do with lift? You can have lift of an object with no Bernoulli. It's simple vector addition. With tables and straws and the like we're talking static, not dynamic pressures. The airplane uses dynamic AND static pressures. Right. In cruise flight (low AOA), I would expect a reduced pressure on the bottom of the wing, though not as low as on the top. The velocity of air across the bottom will drop its pressure, there, too. Right. The AOA matters here. Angle the wing up any significant amount, and over-pressure will build under the wing. Air has mass. Anytime you try to push it out of the way, there will be some reaction. Newton says so. We know this as drag. Hmm...ok, sure. I wouldn't call that drag necessarily. That's like saying that a hydraulic piston assembly has drag. I more prefer to think of drag as laminar fricitional forces of the fluid. Pushing out of way implies that plane doing the pushing is perpendicular to the direction in which pushing is being done (which is true at leading edge of wing). But I guess this is acceptable. But we also know it as lift reaction. A flat plate flying through the air at some tiny angle of attack doesn't have much faster air over the top than the bottom, if any difference at all, yet it will generate plenty of lift. Try this on, if you want to think outside the box: Thinking outside the box is what lead me to refuse to accept hand- waving explanations of aerodynamics from CFI's. The airfoil we know is just that: a foil (device to deceive) to trick the air into flowing over it without breaking up at much higher angles of attack than a flat plate would let us. So the leading edge has to have some radius so the air can get around the corner from the natural stagnation point under the LE at high AOA, and that curve must gradually taper off toward the rear or the now- disturbed air would want to separate and turbulate, and if it did that it would then slow down dramatically, pressure would rise and lift would decrease. But, happily, Newton is still at work underneath so the airplane falls, but not as if the wings fell off. We're still moving forward and the wing is still shoving air out of the way downward, so lift is still generated. Yes this is true, but the explanation in the Jeppensen book is wrong. it defines downwash: downwash: - "the downward deflection of the airstream as it passes over the wing and past the trailing edge" It goes on to say: "According to Bernoulli's principle, the increase in speed of air on top of an airfoil profdues a drop in pressure and this lowered pressure is a component of lift." Ok, we really know that the lift results from what's under the wing no longer being balanced out, but I won't nit-pick this explanation. Next paragraph it says: "In addtion to the lowered pressure, a downwar-backward flow of air is also generated from the top surface of the wing. The reaction to this downwash results in an upward force on the wing which demnstrates Newton's third law of motion." This is plane false. That is *NOT* what Newton said. Newton did not say you could take any action and willy-nilly find what you think is the reaction, and say, "Hey, this looks good, let's use this." Newtons law, in fact, is better stated as reciprocity of force, IMO. This says that, if you take two objects, one apply force to the other, the other, by reciprocity, must appy an opposite force against the first. Newton's law, conbine with F=ma, also yields the notion of conservation of momentum. But getting back to Jeppensen, the downwash, if they mean what's happening on the top surface of the wing, is *not* contributing to lift. Note that they say "results in", but don't explain how. This seems to be typical of books of flight dynamics. I'd like to point something else out regarding Bernouilli's principle. I haven't tried, but I suspect that I could build a contraption that consists of surface where the velocity of air above the surface is much higher than that below, but the pressure above the surface is higher. -Le Chaud Lapin- |
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In fact, if there is a downward component of the air's velocity that
had come from its passage over the upper surface of the airfoil, then there had been an acceleration provided to that air -- acceleration in this case being conventionally defined as the second time derivative of position. Now, if the air is accelerated downward, and it has mass, it means there had been a force applied. The local prime mover is of course the wing, so it must experience an upward force. Maybe you have a different idea as to on what that equal and opposite force is operating on -- I'd be interested in hearing about that. There are a number of basic principles in operation here, be careful not to paint yourself into too tight a corner unless you are quite expert. I am not claiming skill in this area -- physics was a minor a long time ago -- but I remember some of the basics. |
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Tina wrote:
In fact, if there is a downward component of the air's velocity that had come from its passage over the upper surface of the airfoil, then there had been an acceleration provided to that air -- acceleration in this case being conventionally defined as the second time derivative of position. Now, if the air is accelerated downward, and it has mass, it means there had been a force applied. The local prime mover is of course the wing, so it must experience an upward force. Maybe you have a different idea as to on what that equal and opposite force is operating on -- I'd be interested in hearing about that. There are a number of basic principles in operation here, be careful not to paint yourself into too tight a corner unless you are quite expert. I am not claiming skill in this area -- physics was a minor a long time ago -- but I remember some of the basics. The main thing about all this is that both Bernoulli and Newton are complete explanations of lift and will stand alone. In fact they are both explanations of the same thing really as they occur simultainously as lift is being created. The big rub about Bernoulli is that for years Ole' Daniel was raped by text books stating several totally false applications of Bernoulli as fact. The equal transit theory for example, often stated as an explanation for Bernoulli is totally incorrect. The real truth of it is that neither Newton or Bernoulli were dealing with lift at all in their respective work that explains lift. My fondest hope is that someday, pilots will collectively get it together enough to realize that Bernoulli and Newton are not in competition with each other and never have been. Personally though.....I like my old friend Mary Shafer's explanation for lift that blames it on the "lift demons". :-) DH -- Dudley Henriques |
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On Oct 3, 7:29 pm, Tina wrote:
In fact, if there is a downward component of the air's velocity that had come from its passage over the upper surface of the airfoil, then there had been an acceleration provided to that air -- acceleration in this case being conventionally defined as the second time derivative of position. The acceleration is indeed downward. If God declared that all air molecules in the universe must remain still for the sake of USENET explication, and the wing move forward, and you took a snapshot of that picture, there would be a vacuum created above the wing. It would be quite large (not laminar). The floor of this vacuum would be the wing itself. The ceiling would be the underside of an air mass above the entire wing, ready to move downward to fill the void. Now if God said, "Let molecules move!", the air mass above would, indeed, push downward. But they would not be allow to go completely downward. Molecules accelerated from the leading edge of the wing would fly backward, colliding with those coming from above, and the net-effect would be a stream. Now, if the air is accelerated downward, and it has mass, it means there had been a force applied. The local prime mover is of course the wing, so it must experience an upward force. Maybe you have a different idea as to on what that equal and opposite force is operating on -- I'd be interested in hearing about that. The force is coming from the air mass above the wing, the air mass that would be right above the vacuum created if no molecules were allowed to move. That airmass pushes downward, toward the void. This has nothing to do with the wing, except that the wing created the void, and also created high-pressure area at tip of wing causing acceleration of air backwards. There are a number of basic principles in operation here, be careful not to paint yourself into too tight a corner unless you are quite expert. I am not claiming skill in this area -- physics was a minor a long time ago -- but I remember some of the basics. I am not an expert either, but I know enough to know that the explanations I am reading in books are, at best, misleading. Some of them are plain wrong. Note: going to start a new thread so we can get to the bottom of this. And yes, I am certain. ![]() -Le Chaud Lapin- |
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Le Chaud Lapin wrote:
You can have lift of an object with no Bernoulli. It's simple vector addition. 1. You are talking about nature's abhorrence of a vacuum. 2. Vacuum abhorrence is not lift. 3. Airplanes do not generate lift as a result of vacuum abhorrence. ---------- Conclusion: you are not talking about how aircraft generate lift. QED. TheSmokingGnu |
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