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Momentum transfer at microscopic level
long discussion unrelated to improving the article |
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If I understand well, there is a positive net transfer of (upward) momentum from the particles striking the foil. Is this correct? Mark.camp (talk) 19:12, 6 February 2015 (UTC)
Mark.camp (talk) 02:27, 18 February 2015 (UTC) The net force on the foil is zero (unless the machine is manoeuvring). In a billiard-ball model, the balls are deflected downwards in accordance with L=dp/dt. The balls gain downward momentum but the foil does not gain upward momentum. The planet beneath gains the upward momentum as gravity attracts it towards the heavier-than-fluid foil, but the effect on the airflow and on the foil is negligible. Of course, net momentum change of planet + balls = 0. —
(Zapletal writes ->) Mark, "Is there a transfer of vertical momentum to the foil when a single particle with nonzero vertical momentum collides with the foil?" I recall this being discussed before, but can't remember where. The short answer is that there is a big difference between a "Kinetic Theory of Gases" description of Lift, and a "Continuum Mechanics" description. Both give the same end result, but in different ways. In yours and the KToG descriptions, very soon after your particle bounces downwards off the underside of the foil it hits another particle below it, bounces back upwards off it, and then continues to bounce up-and-down between the underlying particles and the foil (this, of course, is greatly simplified...). There are a great many (squillions!) of these exchanges of momentum, and their net result, summed over the whole surface of the foil, is the Lift force. However, in the CM description, these "collisions of particles against foil" are simply called "pressure". There are more frequent collisions on the underside of the foil, so "greater than ambient pressure" there, and less frequent collisions above, so "lower pressure". By definition, the Continuum cannot consist of individual particles, so the only way it can interact with other Bodies is via these "pressure" forces acting at the mutual boundaries. (This ignores Gravitational, EM, etc., interactions, and strictly speaking the interactions are via a "stress tensor", which also models "friction = viscosity".) (End Zapletal) 101.171.255.254 (talk) 04:47, 7 February 2015 (UTC)
(Zapletal Writes ->) Mark, Your last sentence pretty much nails it (in terms of this simplified "billiard ball" model...). For an even simpler version, consider an aerofoil moving at constant horizontal velocity through a vacuum, and above a large massive body such as the Earth. The gravity force between Earth and foil pulls them together, and gives them both equal time-rate-of-change of inwards momenta (ie. d(m.V)). Of course, the lighter foil has the higher dV here, so follows a more curved path (roughly parabolic, concave down). Now picture something like a football bouncing up and down "elastically" (!) between the two bodies. Each time it hits the Earth and bounces back up, it "exchanges" twice its vertical linear momentum with the Earth, and gives it some downward dP (but of very tiny dV). Similarly, each time it hits the underside of the foil and bounces back down, it gives the foil the same upward momentum dP. So answer to your original question is, indeed, YES. End result is that the foil travels along a path a bit like "mmm". The bouncing ball in this model is roughly equivalent to Lanchester's "pillar" from page 9 of his book, ie., "As a whole, the fluid, in the previous section, does not gain or lose momentum any more than does a cast-iron pillar supporting a load." . Adding more detail to the model has many more balls bouncing every which way, which add, in Continuum Mechanics terms, an "ambient pressure" everywhere. But, for this BB model to work there MUST be a time-averaged increase in the number of these balls bouncing between each other in the zone between the Earth and foil. This "increased pressure zone" MUST ALSO travel steadily with the foil, much as the single football does above, or as does Lanchester's "cast-iron pillar". (End Zapletal)101.171.127.235 (talk) 03:01, 8 February 2015 (UTC)
Fluid Dynamic Lift, of the type that is presented in the main article, is a subject that was developed in, and best belongs in, the field of Hydrodynamics. This is the study of idealised, inviscid, INCOMPRESSIBLE, fluids similar to water (hence "hydro"). The main article is currently written mostly from the point of view of Aerodynamic Lift. But, because gaseous air moving in what is commonly called "low-speed, sub-sonic flow" behaves very much like the incompressible liquids of Hydrodynamics, the original Hydrodynamic explanation of FDL works fine here. But an important distinction needs to be made. Whereas gaseous fluids can be modelled as Billiard Balls that are mostly flying freely through a vacuum and only briefly bouncing off each other, in liquids the modelled BBs are ALWAYS in intimate contact with other BBs. (So picture the difference between 10 x BBs bouncing around a big billiard table, and 1,000 x BBs all in contact in a group on the table, but with this group freely deformable, or "fluid".) Thus the BBs in the hypothetical liquid can exert a force on a Body indefinitely, without the BBs ever moving, and without anything ever "exchanging momentum" (eg. "hydro-static" pressure forces). Note that the hypothetical particles that are assumed to make up a "real" liquid (ie. atoms, etc.) are thought to be in a constant "jiggling" motion related to their "heat energy". But so too are the atoms of a solid, and nobody pretends that the atoms of a cast-iron pillar ever need to "exchange momentum" to support a load. Neverthless, the "particles" that make up a hypothetical Hydrodynamic fluid (continuously divisible, so not atoms!) are assumed to possess Inertial mass, so they DO require a force impressed upon them to change their "quantity of motion" (= Newton's term for "momentum"), as per Galileo's Law of Inertia, aka NI. So it takes a force acting over a distance to get this fluid moving, and the fluid then gains momentum and kinetic energy. But, again, these same hypothetical fluid particles can also transmit forces with NO MOTION, or NO "exchange of momentum", whatsoever. Picture a heavy boat floating in a quite pond of water. Or the same boat floating in a pond of very slippery, but stationary, billiard balls. Same-same. (End Zapletal)101.171.213.77 (talk) 02:19, 9 February 2015 (UTC)
1. Semantic quibble first. This "Lift" subject is part of a nested hierarchy, roughly; Classical Mechanics = Rigid-Body-Mechanics + Fluid-Mechanics +..., Fluid-Mechanics = Fluid-Statics + Fluid-Dynamics +..., Fluid-Dynamics = Hydrodynamics + Aerodynamics +..., etc. The explanations of "Lift" in this article come mostly from the field of Hydrodynamics, but they are couched, unfortunately IMO, mostly in Aerodynamic terms. So, the article uses the word "air" too much, rather than the more general "fluid". Note that anything that "flows" is a fluid. Anyway, "Fluid-Dynamics" covers both the individual-particle model (whether the particles be of liquid or gas) and also the continuum model (again, of both incompressible liquids and compressible gases). But "Hydrodynamics" generally only refers to the incompressible continuum model. To stress it again, the Circulation Theory of Lift (ie. the main one presented in this article), is a Hydrodynamic theory. ~o0o~ 2. Mark, I think you are asking, " there is a non-zero rate of momentum exchange between the three bodies , equal in magnitude to the lift. ... So, even though (in the fluid dynamics model) the wing has zero change in vertical momentum, it is exchanging vertical momentum with the air as a single body" Simple answer, NO. There is NO "exchange of momentum" between wing<->fluid, or between fluid<->ground, in the CToL continuum model (which happens to be the best model available for last ~120 years). But you are not alone in this misunderstanding. Certainly most of this Talk page, and some of the others, are devoted to arguing this issue. In brief, in the CToL model of steady flight of a wing, the NET FORCE acting on the wing, namely the sum of downwards-forces (eg. gravity) + upwards-fluid-pressure forces, is ZERO. The force system acting on the wing is in EQUILIBRIUM. Hence "steady" flight. Same for the ground. However, there ARE changes-of-momentum of the various different parts of the continous fluid. These are a result of the pressure field that travels with the wing and supports it. This pressure field terminates at the fluid's boundaries, which include the wing and ground surfaces. The above misunderstanding is, IMO, a result of "fluid" being slippery stuff that offers little resistance to being pushed, so it simply moves out of the way whenever you push it. But then, because of the fluid's slipperyness combined with the MOMENTUM it picked up when you first pushed it, it manages to circle around behind you, and push you forward so you fall flat on your face! <- This is a very non-technical description, but it is the gist of how the CToL maintains the pressure field so it travels unchanged with the wing. (End Zapletal)101.171.127.229 (talk) 05:15, 10 February 2015 (UTC)
(Zapletal Writes->) Mark, Steelpillow's and my explanations most certainly DO differ. Steelpillow, my explanations are based on a long study of the works of the many people who founded this body of knowledge, together with careful checking of the implications of those works to determine how well their predictions correlate with measured observations in the real world. Your explanations, from what I have seen so far, are based on a narrow ideology (eg. "TS"), that is founded on a meager understanding of fundamental principles, that gives NO quantifiable predictions, but which you nevertheless promote by attempting to suppress all alternative viewpoints. I could also mention that your tone is decidedly "uncivil", you seem to be "not-here" to educate or build a better encyclopedia, etc. But I doubt it will make any difference... Doug, I must apologise to you that I am finding "Wiki" a thoroughly futile exercise. Thank you for your (excellent!) efforts so far. But, s jwe;ifgvyubwe w;adly, I think good education is impossible under these conditions. (End Zapletal) 101.170.127.248 (talk) 02:55, 11 February 2015 (UTC)
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Angle of attack
For an asymmetric foil, "angle of attack" can only be defined by arbitrary convention. (The concept is physically meaningless. It is physically meaningful only with respect to the trailing stagnation point, which is justifiably considered the aft point of the chord). The forward stagnation point is not completely defined by the geometry of the foil, but rather by the flow under specified conditions. The point defined, arbitrarily, as the forward point of the chord, has no physical meaning, only an intuitively simple significance.)
I edited two sentences accordingly. Each of these implicitly treated "angle of attack", incorrectly, as a physically meaningful concept in the general case, irrespective of symmetry.75.185.66.0 (talk) 03:07, 10 February 2015 (UTC)
- Except, the first source I opened disagrees. It defines the "chord line" through from the centres of curvature of the leading and trailing edges, and uses this as the baseline for the angle of attack. Yes it is arbitrary in a theoretical sense, but not in an engineering sense. Also, your agonies of pedantry are not a style of writing that sits well with readability. It is easier to start again, so I am undoing your edits. — Cheers, Steelpillow (Talk) 09:55, 10 February 2015 (UTC)
- Different sources define the chord line differently, and so the angle of attack will also vary depending on how one defines the chord line. Is this variance in the strict definition of "chord line" important? I don't think so, especially at this point in the article where it would be premature to go into too much technical detail. Clancy's definition is fine, but it's not the only one and I'm not sure that we are fairly representing the sources by using it without mentioning the others. Since I don't think the reader would be served by going onto a tangent about different definitions of "chord line", my preference is to simply link to the article Chord_(aeronautics) and remove Clancy's definition. I think the diagram to the right is sufficient to get the idea across. I've made the edit - let me know what you think. Mr. Swordfish (talk) 18:19, 10 February 2015 (UTC)
- Yes, thank you, that is a definite improvement. — Cheers, Steelpillow (Talk) 20:32, 10 February 2015 (UTC)
- Different sources define the chord line differently, and so the angle of attack will also vary depending on how one defines the chord line. Is this variance in the strict definition of "chord line" important? I don't think so, especially at this point in the article where it would be premature to go into too much technical detail. Clancy's definition is fine, but it's not the only one and I'm not sure that we are fairly representing the sources by using it without mentioning the others. Since I don't think the reader would be served by going onto a tangent about different definitions of "chord line", my preference is to simply link to the article Chord_(aeronautics) and remove Clancy's definition. I think the diagram to the right is sufficient to get the idea across. I've made the edit - let me know what you think. Mr. Swordfish (talk) 18:19, 10 February 2015 (UTC)
- 75.185.66.0, I agree that "angle of attack" can only be defined by arbitrary convention and that different authors use different definitions. But the place to present that information is not in an introductory section aimed at lay readers in an article about aerodynamic lift. The minor differences among the differing definitions would be a distraction from the discussion and would not foster better understanding by the intended audience. There are articles on the angle of attack and chord line - either would be a better place for this level of detail. Mr. Swordfish (talk) 18:41, 10 February 2015 (UTC) Mr. Swordfish (talk) 18:41, 10 February 2015 (UTC)
I did not explain my concern very well.
Please be assured that I understand that chord has a conventional definition, or more than one, which is/are very useful in engineering, even though they only apply to common commercial configurations (not a Flettner rotor, for example, or a blob, or a foil with a sharp edge somewhat aft but not aftmost). My problem with it is NOT that it's not practically useful, say in an engineering handbook or product catalog. But this article is trying to explain lift, conceptually. Introducing it in the introduction is not just harmless but irrelevant, but I think highly misleading, because it amplifies a common, highly intuitive tendency to misunderstand lift. It reinforces the view that lift is like a billiard ball striking another off-center. In the billiards case, it is correct to believe that the forward-most point of the struck ball is a physically meaningful chord end-point.
We know that there is a common misconception that lift results from air striking the "bottom" of a "tilted" plane--with the "leading edge" being the farthest point forward and the trailing edge being the farthest aft, just as in the case of a billiard ball or a thin planar surface. The intuitive belief is that the airflow must split at this point, and that all points aft of this on the bottom are obstructing the flow, and thus creating high pressure, and all points aft of this on the top being in a condition of vacuum.
We know that this conception is completely without theoretical justification, and is factually incorrect (in the case of a barn door, even if we use the simplistic complex analysis model, the airflow splits well aft of the end of the "chord"!)--it is the misconception that we are trying to replace with a correct account of the actual pressure and velocity fields, and a correct account of why they occur. The aft stagnation point indeed happens to be the aftmost point on an ordinary commercially available wing, but the intuitive conception that it is the stagnation point BECAUSE it is the aftmost point is completely incorrect; in fact, the Kutta condition is the explanation, and the sharpness of the point, and not the fact that it is aftmost, is the relevant fact. And the idea that the foremost point is a stagnation point is not only based on completely spurious reasoning, it also happens to be completely incorrect experimentally and also inconsistent with every physical model from complex analysis up to and including the most complete differential equation.
My concern is that presenting an arbitrary engineering convention about how to define "tilted" in the intro, as if it were somehow related to the subject of lift, strongly encourages this misconception. ~~ — Preceding unsigned comment added by Mark.camp (talk • contribs) 02:51, 13 February 2015 (UTC)
- "it is the misconception that we are trying to replace with a correct account..." - stop right there. No we are not. This is one of the commonest misconceptions by PoV editors as to what Misplaced Pages is about. We are trying to build and encyclopedia according to the WP:FIVEPILLARS and other goodly policies and guidelines. Most relevant here, we seek what is often called "verifiablility not truth". Where are the reliable sources (WP:RS) that claim this is a common misconception that must be addressed, and that the standard introductory texts do in fact explicitly debunk it? — Cheers, Steelpillow (Talk) 15:38, 13 February 2015 (UTC)
- I'm not quite sure how this discussion sprung from the description of "angle of attack" in the article. It's a simple geometric definition, not a description of the physics.
- From a pilot's perspective, AOA is very important to the subject of lift. In Stick and Rudder, Langeweische spends most of the book talking about it. The Lift coefficient is dependent on AOA. If it gets too high, the aircraft stalls.
- When you say "tilted", are you referring to, "when an aircraft is climbing, descending, or banking in a turn the lift is tilted with respect to the vertical"? That sentence has nothing to do with angle of attack, but arises from the fact that lift is, by definition, perpendicular to the relative airflow over the wing. Burninthruthesky (talk) 16:07, 13 February 2015 (UTC)
- I think what Mark is trying to say is a)it is not necessary to introduce the notion of chord line at this point in the article, and b) doing so is misleading because it may re-enforce by implication some common misconceptions.
- I agree with point a) to some degree. The article used to say the angle of attack is the angle between the foil and the oncoming air; recently the definition was made more precise by introducing the notion of chord line and linking to that article. My take is that it was fine before, but that it's a bit stronger with the more precise definition.
- As for point b), I suppose one could imply all those incorrect notions of which Mark speaks from our addition of four little words (" the chord line of"), but it would take quite a bit of imagination. I think all of the misconceptions mentioned by Mark are either directly addressed and corrected by the article, or at least not re-enforced. Perhaps material could be added elsewhere to address Mark's concerns? for instance, we don't cover the "skipping stone" misconception - perhaps we should. Mr. Swordfish (talk) 16:45, 13 February 2015 (UTC)
- Mr Swordfish, I am sorry to say, expresses what I was trying to say just a wee bit better than I did. So I will start by taking his cue and asking this: what is the purpose of introducing the notion of chord line (which is useful only in establishing an arbitrary point of reference for purposes of communication, for example in operator's manuals and marketing materials) at this point of the article, which is not intended to be an operator's guide for some commercial product, but a general explanation on lift ? Mark.camp (talk) 04:40, 14 February 2015 (UTC)
- I agree that for a cambered airfoil, the concept of chord line is arbitrary. In many analytical situations we are interested in the change in angle of attack rather than the absolute value, and in these situations it doesn't matter how the absolute values are determined. In analytical situations where we want to avoid the arbitrariness of a chord line it is customary to measure the angle of attack relative to the zero-lift line. Dolphin (t) 05:37, 14 February 2015 (UTC)
- The main article on angle of attack covers these various reference lines in more detail. If it's felt that mentioning the "chord line" is confusing, I've no objection to a simpler description in this article. In that case perhaps an explicit "main article" link would be helpful. Burninthruthesky (talk) 08:23, 14 February 2015 (UTC)
- So, let's see how reliable sources treat this subject. Here are the three elementary treatments that I have handy:
- Kermode; Mechanics of flight, 1972 edition, pp 75-76: Titles a section "Chord line and angle of attack", then discusses the chord line before turning to the angle of attack.
- Clancy; Aerodynamics, 1975, p 56: introduces the chord line and then, lower in the same section, defines the angle of attack in terms of the chord line.
- Simons; Model Aircraft Aerodynamics, 1978, p 10: Introduces the angle of attack, then defines it with respect to the chord line, then defines the chord line - all within a single paragraph.
- That list is uncensored - I didn't pull any books that disagreed with a PoV or anything.
- It is clear to me that if we do not know what the angle of attack is, then any statement about the angle of attack of a cambered aerofoil is well nigh meaningless. A Misplaced Pages article is expected to provide, as a minimum, the information to make some kind of sense of its narrative, and to link to more detailed explanations where appropriate. As an example of the conceptual semantics involved here, the accompanying illustration finds it necessary to depict the chord line in order to give adequate realisation to the angle of attack. The text needs to do the same. As you can see, the reliable sources I found all support that view. None is followed immediately by addressing any confusion over the stagnation points, though Kermode discusses the more direct confusion over the difference between angle of attack and angle of incidence. Unless anybody can find sufficiently weighty sources to the contrary, these sources show that we need to introduce both topics in close association and not get distracted by indirect confusions over other topics. Therefore, rather than deleting all mention of the chord line, we should actually reintroduce its definition. — Cheers, Steelpillow (Talk) 11:58, 14 February 2015 (UTC)
- So, let's see how reliable sources treat this subject. Here are the three elementary treatments that I have handy:
- The main article on angle of attack covers these various reference lines in more detail. If it's felt that mentioning the "chord line" is confusing, I've no objection to a simpler description in this article. In that case perhaps an explicit "main article" link would be helpful. Burninthruthesky (talk) 08:23, 14 February 2015 (UTC)
- I agree that for a cambered airfoil, the concept of chord line is arbitrary. In many analytical situations we are interested in the change in angle of attack rather than the absolute value, and in these situations it doesn't matter how the absolute values are determined. In analytical situations where we want to avoid the arbitrariness of a chord line it is customary to measure the angle of attack relative to the zero-lift line. Dolphin (t) 05:37, 14 February 2015 (UTC)
- Mr Swordfish, I am sorry to say, expresses what I was trying to say just a wee bit better than I did. So I will start by taking his cue and asking this: what is the purpose of introducing the notion of chord line (which is useful only in establishing an arbitrary point of reference for purposes of communication, for example in operator's manuals and marketing materials) at this point of the article, which is not intended to be an operator's guide for some commercial product, but a general explanation on lift ? Mark.camp (talk) 04:40, 14 February 2015 (UTC)
The talk page is not a forum for general discussion
I would like to remind the participants of relevant wikipedia policy:
- Discussion forums. Please try to stay on the task of creating an encyclopedia. You can chat with people about Misplaced Pages-related topics on their user talk pages, and should resolve problems with articles on the relevant talk pages, but please do not take discussion into articles. In addition, bear in mind that talk pages exist for the purpose of discussing how to improve articles. Talk pages are not for general discussion about the subject of the article, nor are they a help desk for obtaining instructions or technical assistance. Material unsuitable for talk pages may be subject to removal per the talk page guidelines. If you wish to ask a specific question on a topic, Misplaced Pages has a Reference desk, and questions should be asked there rather than on talk pages.
See WP:FORUM. I would ask that participants restrict discussion to that related to editing the article's content and that lengthy discussion outside the context of how to improve the article should be moved to user talk pages. Mr. Swordfish (talk) 21:26, 17 February 2015 (UTC)
- I would heartily endorse Mr. Swordfish. Please can users confine off-topic chat either to their own user talk pages or entirely off-wiki. — Cheers, Steelpillow (Talk) 21:39, 17 February 2015 (UTC)
For me this section "Angle of Attack" shows not as a separate article but as a continuation of another section, "Momentum transfer at microscopic level". Anyone else have this problem? I checked the syntax and it seems that the same tokens, leading and trailing instances of "==", are the same. Mark.camp (talk) 01:39, 18 February 2015 (UTC)
- Mark, are all your latest questions aimed at improving this article or just for your own satisfaction? If they are not aimed at improving the aticle then it is time to move the convesation elsewhere. — Cheers, Steelpillow (Talk) 09:36, 18 February 2015 (UTC)
Suggested text on momentum transfer
Re:
- "Some of the air passing the airfoil has downward momentum imparted to it at a rate equal to the lift."
The text complicates the discussion by dividing the air arbitrarily into two bodies, each of which must then be defined and analyzed. The subject gets extremely complex and difficult to explain.
Why not just directly apply Newton's second law, expressed in terms of rate of momentum change between two bodies, to the two bodies we are discussing, the foil and the air? I suggest this text.
- "There is an exchange of vertical momentum between the foil and the air."
This raises some issues.
First, it is a controversial assertion here at the moment, and the controversy would first need to be resolved. I attempted to prove the assertion in a subsequently collapsed Section. I was waiting for a response correcting or accepting my proof. (I assume that that thread can still be responded to. Otherwise, I will duplicate the proof in this Section.)
Second, it would need authoritative references.
Third, assuming the assertion is correct, the article would need to address, somewhere, a very difficult and subtle issue: why does the continuum theory, which is critically important in the settled science and the article, and otherwise correct, imply that the momentum exchange is zero? I attempt to show the source of the incorrect result in detail in the collapsed post.
Fourth, the remainder of the article would need to be made consistent with the sentence.
Fifth, the momentum balances of the foil or craft, air and earth would need to be addressed in terms consistent with the above.
Mark.camp (talk) 23:16, 18 February 2015 (UTC)
- I'm not gone, yet at least. Back to Mark's question.
- I assume Mark originally brought his question up not just as a matter of general interest, but because he thought it might impact what should be included in the article. So it seems to me to have been a bit arrogant to judge the whole "Momentum transfer at microscopic level" section to be "unrelated to improving the article".
- That said, Mark's apparent contradiction between the microscopic and continuum views isn't really a contradiction. Both ways of describing the flow are correct and consistent with physical reality. We have the appearance of a contradiction only if we use the word "momentum" indiscriminately. It is resolved when we note that "momentum" doesn't generally refer to the same thing in the continuum description as it does in the molecular description.
- In the microscopic view, "momentum" is associated with the motions of molecules, including the random thermal part of the motion. The random thermal motion has no preferred direction, and in gas flows at low Mach number, the thermal motion predominates, with the "flow" looking like a relatively small directional "drift" superimposed. At any stationary solid surface, the average (continuum) velocity of the gas goes to practically zero, so sufficiently close to the surface of an airfoil the only molecular motion we see is random thermal motion. The bouncing of individual molecules against the surface is diffuse, not specular, and individual bounces are not elastic (an individual molecule can either lose energy to the surface or gain energy from it), so that incoming and outgoing perpendicular momentum are not usually equal-and-opposite for any one molecule. But on average over many molecules, incoming and outgoing perpendicular momentum are equal-and-opposite, provided the surface and the gas are in thermal equilibrium. So the surface pressure is the result of many molecules per unit time having the perpendicular component of their thermal momentum reversed, on average, in their collisions with the surface, and the thermal momentum fluxes of incoming molecules and outgoing molecules account for half of the pressure each.
- "Momentum" in the continuum description is based on the continuum velocity of the fluid. As noted before, all components of the continuum velocity near the surface are practically zero, and there is no change or "exchange" of continuum momentum taking place as a result of exerting pressure on the surface. The pressure in the continuum description is just a force per unit area, and nothing needs to be said about the details of how molecules produce the force. Whether pressure consists of forces transmitted between molecules in direct contact with their neighbors, as in a liquid, or is produced by bounces of isolated molecules, as in a gas, doesn't matter in the continuum description. The representation of the pressure as a force per unit area in the continuum momentum and energy equations is the same regardless of whether the fluid is a liquid or a gas.
- If we take the molecular view of upward lift on an airfoil, the lower surface is imparting a downward change to the thermal momentum of molecules at a greater average rate than the upper surface is imparting an upward change, so there is a net downward imparting of thermal momentum (Mark's "10,000 N") to molecules impacting the surface. On the other hand, nothing is happening to the vertical continuum momentum locally at either surface, so the net rate of change of vertical continuum momentum is practically zero for the fluid very close to the upper and lower surfaces (Mark's "0 N"). In the actual flow field, vertical momentum is imparted to the flow over an extended region around the foil, and practically none of it is associated with molecules that acquired it directly through collisions with the surface. So Mark's "10,000 N" and ""0 N" refer to two different things, and are both correct. There is no contradiction.
- Further points worth noting:
- For atmospheric flight at ordinary scales, the molecular mean free path is extremely short, and the continuum theory is highly accurate. The molecular description offers practically no advantage in fundamental accuracy.
- If you know the density and temperature locally, the molecular theory can tell you the pressure. But the molecular theory is practically useless for predicting the density or pressure variations in ordinary aerodynamic flow fields. The continuum theory is the only choice for actual predictions. And for gasses at low Mach numbers, or for liquids, the continuum theory can predict the pressure differences without having to deal explicitly with the density differences.
- The continuum approach is also the only workable choice for qualitative explanations at the flow-field level. So if Mark was thinking that the microscopic description should perhaps play a role in explaining lift in the article, I think the correct response would be "No, it shouldn't". The molecular description is practically useless for understanding why ordinary flow fields behave as they do. This makes sense when you realize that at a given Reynolds number the flow field described in dimensionless terms is the same regardless of whether the fluid is a gas at low Mach number or a liquid. At the flow-field level, the only properties of the fluid that matter are the density and viscosity, which are macroscopic quantities. The details of the molecular motions have no effect on the global motion and thus provide no help in understanding it.
- I agree with Mark that the current quantitative statement unnecessarily "complicates the discussion". But his suggested fix misses on two counts: 1) There is no vertical momentum imparted to the foil in level flight, and 2) To be correct in general, his version of the statement has to be referring to the microscopic version of momentum, which for the reasons I discussed above isn't how aerodynamics analyses and explanations are constructed. Citable sources that do it that way, and do it correctly, are nonexistent.
- So no wholesale reworking of the article is in order. But Mark's problem with The Statement would be alleviated, and the article would be improved (as I've said repeatedly) if the current quantitative version were replaced by a qualitative version, as in Langewiesche. I don't think we're done with that discussion. More later.
- Thanks much, Doug. I will need to study your latest to understand it, but unfortunately will not be replying as I'm excusing myself from the discussion. This community has become a very unpleasant place for conversation, and I admire your persistence in remaining engaged in the hopes of improving the article for its users.
- Mark.camp (talk) 23:00, 19 February 2015 (UTC)
- To reiterate a point made many times: Misplaced Pages does NOT document what its editors believe to be true. Misplaced Pages documents what reliable sources tell us is true (see WP:VERIFICATION and WP:RS). This conversation is paying no attention whatever to sources and as such it is mere off-topic chat masquerading as an edit discussion. If folks don't shut up I'll take this to ANI in my own way. — Cheers, Steelpillow (Talk) 07:41, 19 February 2015 (UTC)
- @Steelpillow, I did not alter the article to agree with what I believe to be true, so you are preaching to the choir. This conversation is based on what I as an ordinary (non-expert) consumer find to be confusing about the current text, and until that is clarified by the experts here, and the text improved if that is deemed necessary, it is perfectly legitimate. Misplaced Pages policy doesn't require a person who finds article text confusing to provide any sources in the context of a Talk page...otherwise, no user would ever be permitted to raise such an issue--who would ever have written a paper about the fact that some Misplaced Pages text is confusing to one individual? This discussion is very much on topic, and my intention is not to masquerade about anything.
- However, since you and others seem to find my attempts to help offensive, and you question my motives rather than just my words, I will not pursue either of the two discussions I started any further.
- Mark, if I misunderstood your motives, then I must of course apologise. But it makes no practical difference. The interminable edit discussion on the Newtonian model was closed. It should not be reopened gratuitously unless new sources are found to support revisiting the consensus finally reached. WP:DISRUPTION explains that "Editors may be accidentally disruptive because ... they lack the social skills or competence necessary to work collaboratively. The fact that the disruption occurs in good faith does not change the fact that it is harmful to Misplaced Pages." Also, "In some cases, editors have perpetuated disputes by sticking to an allegation or viewpoint long after the consensus of the community has decided that moving on to other topics would be more productive. Such behavior is disruptive to Misplaced Pages." This is where we are now on the matter of Newtonian lift. You are of course welcome to pursue these discussions on your own user talk pages, such as User talk:Mark.camp or User talk:J Doug McLean, and to invite other editors to contribute. Unless Zapletal creates themself a user account, they will have to make do with someone else's, as their IP address is not static (Even there, excessive abuse of other editors may lead to more formal sanctions such as IP blocking). If anybody would like some help on using Misplaced Pages's user pages more effectively, I will be glad to do what I can. — Cheers, Steelpillow (Talk) 10:37, 20 February 2015 (UTC)
- The reason I collapsed the discussion is that I did not see anything concrete regarding how the article might be changed. I'm sure you've been to meetings where discussion goes off on a tangent - at some point someone needs to bring it back on-topic. In structured meetings, it's required that some specific motion be on the table before any discussion takes place. I don't think we need that level of structure here, but long posts that don't relate to actual proposed edits don't get us anywhere - they are fine on user talk pages, but let's try to stay focused here.
- You suggest replacing the current quantitative version with a qualitative version as in Langewiesche. Can you provide sample text?
- I do not take offense at your participation, and think your input is valuable. In particular, if you find the text of the article confusing we should take that criticism seriously. It is not enough that the article simply be technically correct, it needs to be written in a way that ordinary non-experts can understand.
- My apologies if you took my recent attempts to focus the discussion the wrong way.
- As a housekeeping note, I'll be away from the internet for a while, so don't take it the wrong way if I don't respond immediately. Mr. Swordfish (talk) 20:40, 20 February 2015 (UTC)
Berriman
I just added a cite to Berriman's 1913 book on Aviation on the matter of Newtonian lift. In the quotation I cite, "Thus, the wing in flight continually accelerates a stratum of air downwards, and must derive a lift therefrom", the italicisation of "must" is his own. Berriman was a respected authority of his day, and writings of his published in Flight through 1912-13 make it abundantly clear that he was well aware of Lanchester's work. His book also received positive reviews. I have found not the slightest hint or suggestion of any historical controversy over the quantification of Newtonian lift at this time, least of all between Berriman and Lanchester. — Cheers, Steelpillow (Talk) 16:55, 2 March 2015 (UTC)
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