AOPA Flight Training - WHAT ARE THEY THINKING??????

Capt. Geoffrey Thorpe

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Light and Sporty Guy
They must have known that I finally broke down and sent in the money for a paid membership...:mad3:

My letter to the editor:

It was with great despair that I read “The magic of lift” from the January 2009 issue of AOPA Flight training – I find that the “theory” presented is based primarily on misunderstandings, bad assumptions and erroneous mythology.

Let's look at a couple of examples.

The author writes that “Bernoulli himself would probably disagree with [Bernoulli's theorem] when it is applied to the air. He stated that his theorem was for a 'non-compressible fluid' and we all know that air is compressible.” Rubbish. Yes, air can be compressed, but in the context of sub-sonic airfoils, air behaves quite closely to a uncompressable, ideal gas. Let me quote Abbot and Von Doenhoff (Theory of Wing Sections – chapter 9, Effects of compressibility at subsonic speeds)
“The wing-section theory and experimental data presented in the preceding chapters are applicable to conditions where the variation of pressure is small compared to the absolute pressure. This condition is well satisfied when the speed is low compared with the speed of sound. “


Then, in the article, I read: “the air traveling over and under the wing meets at the trailing edge of the wing at the same time.” This has to be the most repeated, most completely wrong aviation myth that has ever existed. In fact, if it were true, aircraft as we know them would not be able to fly – the difference in distances over the top and bottom of the wings simply isn't enough to create the necessary difference in velocities to generate the required lift. Let me direct you to a NASA web page that is devoted to correcting this nonsense: http://www.grc.nasa.gov/WWW/K-12/airplane/wrong1.html In addition to the explanation, this page includes a wing simulation appropriately using the Euler equations http://www.grc.nasa.gov/WWW/K-12/airplane/eulereqs.html

Also, if the “equal transit” theory were true, wouldn't it be impossible to fly an aircraft with a symmetric airfoil or to fly inverted in an aircraft with a more typical asymmetric airfoil? I can assure you that not only is it possible, I have done both.


Quite frankly, I was exceptionally disappointed with the article.
Comments?
 
Well, that's still what the FAA teaches and students are tested on, so what is AOPA supposed to do?

Really? The FAA teaches the "boy molecules and girl molecules all have to get to the trailing edge at the same time" nonsense? Too bad. (It's been a Loooooooooonnnnnnnnnggggggg time since I took any FAA test so I can't say what is or isn't on them):frown2:

Edit: I just skimmed through chapter 3 of the "Pilot's Handbook of Aeronautical Knowledge" - I'm not seeing any reference to the equal transit nonsense. (But I did see where they listed the same NASA web page I referenced.) Got a pointer to where they do use it?
 
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Well, they do teach that higher velocity along the upper surface of the wing creates lower pressure. I tend to think it's the other way around, but I know it's a relative thing depending on your point of observation.

But at least in the latest PHAK, they get into much more detail and cover the Magnus effect and admit that air deflected from the bottom of the wing generates lift too.
 
Well, they do teach that higher velocity along the upper surface of the wing creates lower pressure. I tend to think it's the other way around, but I know it's a relative thing depending on your point of observation.

But at least in the latest PHAK, they get into much more detail and cover the Magnus effect and admit that air deflected from the bottom of the wing generates lift too.

Yup...I was totally confused wondering how the "boy and girl molecules" got to the trailing edge of the wing at the same time.

Now I know that is NOT what happens, but I did for a LONG time.
 
I remember suffering through some of those early explanations of how lift is generated. Thank you for posting the proper references. Never could understand how an airplane could fly upside down back then. But helicopters could only do it one time; so, I was good.

In pilot gatherings, you can tell which pilots suffered through those early definitions; they have nervous twitches and their eyes narrow or become uneven in look "the Jack Elam" syndrome when the subject is raised. See, early on, they were wide eyed, open minded and might even of had some intuitive understanding of how lift worked; then, after exposure to voluminous amounts of FAA material and memorized written tests were required, they slowly began to twitch as they tried to block out what made sense, and memorized material to pass the test! Some really bad cases are evident when the pilot's left or right shoulder rises, his head turns to the side of the raised shoulder, he twitches and he bumps the other side of his head near his ear; like he's trying to knock something out the other ear: that being meaningless data he had to memorize that interferes with clear thought.

When you see someone doing that, have sympathy; they may still be trying to block out correct understanding in case they have to pass another test!!

Best,

Dave
 
I remember suffering through some of those early explanations of how lift is generated. Thank you for posting the proper references. Never could understand how an airplane could fly upside down back then. But helicopters could only do it one time; so, I was good.

Now, that's funny...

It really is hard to explain how wings work. The best explanation I've ever seen was actually in a sailing book ("The Art and Science of Sails"). But telling people stuff that is just plain wrong is just plain wrong...
 
Read the first chapters of "Stick and Rudder."

What Wolfgang Langewiesche had going for him is that he didn't have to dispel Bernoulli in 1938.
I have a student who has been reading that book. It took a sixty-year old writing to convince him it was a good idea to keep the nose down.
 
Both theories are in the written for the FIA (the lower pressure on top as well as the downward deflection).

I've seen many different presentations on the reason why wings create lift including the Bernoulli principal, air hitting the bottom of the wing and deflecting downwards, as well as the air flowing over the camber of the wing and at an angle downwards behind the wing which creates lift. It can be rather confusing. There are many books and articles out there that mention each of these theories but I have to say, I wish they would provide a thorough reasoning for either why or why not these theories are true (other than the Bernoulli principal). I'm not one for being completely happy with half truths.
 
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I have a student who has been reading that book. It took a sixty-year old writing to convince him it was a good idea to keep the nose down.

It's amazing how clear he makes it, even speaking from 60 years back... there were a few things I also didn't quite get until his book turned the lights on. :D
 
I've seen many different presentations on the reason why wings create lift including the Bernoulli principal, air hitting the bottom of the wing and deflecting downwards, as well as the air flowing over the camber of the wing and at an angle downwards behind the wing which creates lift. It can be rather confusing. ..... I wish they would provide a thorough reasoning for either why or why not these theories are true (other than the Bernoulli principal). I'm not one for being completely happy with half truths.
Tristan, they are all true. Mostly they are just different ways of explaining the same phenomenon. Google Coanda Effect for an explanation of the highlight above.
 
Perhaps they can explain whether a plane can take off from a conveyor belt that's moving.....
 
Well thanks a lot. Here I've been flying for years and I've always thought that I was experiencing some kind of miracle every time I went flying. Now what? Next thing you know, someone is going to tell me that Santa is really my parents.
 
Both theories are in the written for the FIA (the lower pressure on top as well as the downward deflection).

I've seen many different presentations on the reason why wings create lift including the Bernoulli principal, air hitting the bottom of the wing and deflecting downwards, as well as the air flowing over the camber of the wing and at an angle downwards behind the wing which creates lift. It can be rather confusing. There are many books and articles out there that mention each of these theories but I have to say, I wish they would provide a thorough reasoning for either why or why not these theories are true (other than the Bernoulli principal). I'm not one for being completely happy with half truths.

Ok. This is all Tristan's fault. She is the one waving a red flag in front of the bull...

So if you don't like what I've attached, blame Tristan. She made me do it.

(It's in PDF form on account of what I ain't smart enough to put the pictures in the right place otherwise (or is it that I am too lazy to figure it out?))
 

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I'm still working on trying to understand what you wrote so bear with me. First off, I can see that air has the capability of wrapping around a ball in a spin if nothing else, although what I dont get is how you can have a complete rotation of air around a flat plane and go in the opposite direction?

So the airfoil is there for at least three reasons: deflection of air downwards as it curves over the top, provides the venturi and less pressure effect, as well as improve stall characteristics by providing the curve so air doesnt separate as quickly during high AOA.

Oh and you never mentioned the theory about how it hits the bottom and is deflected downwards. :D Although thats probably part of Newton's Action/Reaction theory.

If these things are true, it would be nice to find a book as a reference that links them together instead of explaining just the Bernoulli effect and sometimes mentioning Newton. Hopefully I didn't just miss it all these years. I think the main reason that most miss this is that pilots, CFIs, and students are usually not physicists and try to find the easiest/quickest way of describing an often confusing topic.
 
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OK, now... let's explain why LIFT=WEIGHT when the airplane is climbing, level, and descending.

For a student who never got basic physics and the concept of acceleration versus steady state, it's really tough.
 
Way to go Geoff! I'm an AE, and you are spot on! The bunk that 'the molecules meet at the TE' drives me nuts!

ANY non-symmetrical object in an airflow creates circulation, and therefore lift (a force perpendicular to the incoming airflow). Even symmetrical objects, like a baseball, can be made non-symmetrical by spinning them, especially if the surface is rough. Pitchers would have a tougher time pitching a curve with a Cue ball.

Creating lift is easy. Not creating Drag is the tough part. That is the main focus of airfoil design.

What I tell students is:

Airplanes go up because they make air go down. Period. (Newton's law).

The way they make air go down is more involved and elegent - Bernoulli's law. The upper surface of the wing does most of the work, creating a partial vacuum and sucking the passing air downward. The bottom of the wing helps by deflecting the air down as well. The net result is the air behind the wing is redirected downward. When the angle of attack gets too high, the airflow separates from the upper surface which kills the vacuum on the upper surface, so lift goes down (less redirection taking place).
Apply as appropriate to the wing, tail, propeller...
It's simple, accurate, and seems to be well understood.
 
Airplanes go up because they make air go down. Period. (Newton's law).

Really?
Is that it?
Seriously?

No sarcasm. I read all of your post. It almost seems <gasp> understandable by my pea-sized brain now.

Huh. Go figure...
 
OK, now... let's explain why LIFT=WEIGHT when the airplane is climbing, level, and descending.

For a student who never got basic physics and the concept of acceleration versus steady state, it's really tough.
True -
Any time you are traveling in a Straight Line, at a Constant Velocity, all forces are balanced (Lift=Weight, Thrust=Drag). The direction of the straight line (level, up, down) is immaterial.

Unbalanced forces means ACCELERATION, which means either Direction or Speed are CHANGING.

A lot of people associate going up with slowing down, and going down with speeding up, so the concept of climbing or descending at a constant velocity seems unnatural. But in airplanes we do it all the time!
 
Really?
Is that it?
Seriously?

No sarcasm. I read all of your post. It almost seems <gasp> understandable by my pea-sized brain now.

Huh. Go figure...
Seriously!
I know, it destroys the 'superhuman' part of flying...
Then I tell them the real mystery of flying is how to sound cool when talking on the radio. :D
 
I'm still working on trying to understand what you wrote so bear with me. First off, I can see that air has the capability of wrapping around a ball in a spin if nothing else, although what I dont get is how you can have a complete rotation of air around a flat plane and go in the opposite direction?

So the airfoil is there for at least three reasons: deflection of air downwards as it curves over the top, provides the venturi and less pressure effect, as well as improve stall characteristics by providing the curve so air doesnt separate as quickly during high AOA.

Oh and you never mentioned the theory about how it hits the bottom and is deflected downwards. :D Although thats probably part of Newton's Action/Reaction theory.

If these things are true, it would be nice to find a book as a reference that links them together instead of explaining just the Bernoulli effect and sometimes mentioning Newton. Hopefully I didn't just miss it all these years. I think the main reason that most miss this is that pilots, CFIs, and students are usually not physicists and try to find the easiest/quickest way of describing an often confusing topic.

Get a copy of "An Invitation to Fly" and read Chapter 2.

Your 'three reasons' are all the same thing! The upper and lower surfaces of the 'airfoil' (wing, baseball, flat plate, ...) are acting as a 'system' - the upper and lower surfaces don't act independently. The airfoil creates pressures, both low (on the upper surface) and high (on the lower surface). The net result is that air is deflected (action) which creates Lift (reaction) in accordance with Newton's Law.
The shape of the airfoil is designed to get the most deflection for the least drag. The 'proper' shape is a function of speed, which is why there are flaps and slats.
 
I'm still working on trying to understand what you wrote

Well good luck with that LOL
First off, I can see that air has the capability of wrapping around a ball in a spin if nothing else, although what I dont get is how you can have a complete rotation of air around a flat plane and go in the opposite direction?

Well, lets stick with the ball. If it is spinning and not moving, then the air goes all the way around (and around (and around)). But when you chuck the ball at any speed, the spin of the ball slows the air down on the forward moving side and speeds it up on the backwards moving side - the circulation doesn't actually result in a flow going all the way around (well, except for perhaps for a couple molecules worth at the surface). Think of the circulation and the straight line flow as being two theoretical flows. You take those two flows and add them together (accounting for the speed and direction at each point) to come up with the real life air flow that doesn't look like either the linear or circulation flows.

Same thing with the wing - you sum up the two theoretical flows to end up with a real life flow that looks something like figure 3 (after making allowances for my bad artwork :smile:)

attachment.php


So the airfoil is there for at least three reasons: deflection of air downwards as it curves over the top, provides the venturi and less pressure effect, as well as improve stall characteristics by providing the curve so air doesnt separate as quickly during high AOA.

The venturi effect is the faster = lower pressure. You get that with a flat plate airfoil as the air accelerates over the top.

Oh and you never mentioned the theory about how it hits the bottom and is deflected downwards. :D Although thats probably part of Newton's Action/Reaction theory.

Sorry, I'll try harder next time...

If these things are true, it would be nice to find a book as a reference that links them together instead of explaining just the Bernoulli effect and sometimes mentioning Newton. Hopefully I didn't just miss it all these years. I think the main reason that most miss this is that pilots, CFIs, and students are usually not physicists and try to find the easiest/quickest way of describing an often confusing topic.

I really like the explanation in "The Art and Science of Sails" Tom Whidden and Michael Levitt. I assume you probably wouldn't want to buy that one for the one chapter in the whole (expensive) book - unless you want to learn about trimming a spinnaker... If you can't find it in a local library, drop me a note and I can loan you my copy.
 

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They must have known that I finally broke down and sent in the money for a paid membership...:mad3:

My letter to the editor:

Apparently I wasn't the only one who complained - the AOPA response:

Thank you for your letter to AOPA Flight Training, and for taking the time to share your concerns about Deon Christensen's article in the January 2009 issue. Owing to the volume of letters we've received on this particular article, we may not have space to publish your comments, but we appreciate your opinion.
 
This caused a more in depth discussion of lift on another board. Here is one response that discusses Bernoulli in depth, but pretty well says it's much better to keep it simple for most pilots <g>

Let me know if you'd like to see the rest of the post.

Best,

Dave

es, I can hear the groans out there. First, please, if you reply to this
(and it's OK not to), remember to trim it down before posting.
I come to praise Bernoulli, not to bury him, his dad or his uncle. In the
periodic Bernoulli lift debates on rec.aviation.<pick your favorite> there
is always a great deal of heat generated. Personally, I believe that most
schoolkids (and pilots) are best served by a pure Newtonian description of
air being forced downward (and lots of it) instead of a discussion of
differential pressures and Bernoulli, and I'd like to briefly describe why
in a qualitative and historical way. In short, it's because most of you guys
aren't ready for it and I think it hinders, not helps, the understanding of
what is going on. And, I should mention, I am also not competent to apply
Bernoulli's equations to *any* real system today, either. It is not a tool I
use, and I also make no claim to understand the nuances of lift of a real
wing in real air.

When you first study physics as a schoolkid you do very simple problems.
Basic time, speed and distance problems like you might get in fifth grade
math word problems, or the FAA knowledge exam route planning questions.
Motion in one dimension. In a traditional high school physics class you
might get bombarded by coordinate systems and transformations that expect a
budding knowledge of trigonometry, and you learn some basic Newtonian
physics. More detail of motion in one dimension. Two dimensions, even.
Conservation of energy, conservation of linear and rotational momentum. Neat
stuff, often relying on fictions such as massless pulleys and ropes,
frictionless bearings and other flights of fancy, and there is a great deal
of insight that can be gained with some elementary one variable differential
Calculus (Calculus, not coincidentally, is also something Newton figured out
first).

Go on to college to study more science and you get more of the above your
freshman year. Including more massless and frictionless pulleys. Digging out
my old Halliday & Resnick "Physics", there were about 650 pages devoted to
25 chapters that I think were covered in the first year. "Bernoulli's
equation" is presented in chapter 18 but only in a simplified form that
assumes steady and incompressible flow. Chapter 18 (22 pages) is an
introduction to fluid dynamics, but it's mostly very basic stuff devoid of
calculus, in part because none of the frosh involved had yet taken any
significant multivariable calculus, or how to actually make any sense of
difficult differential equations (or diffyQ's as we'd call them),
multivariable or not. The fluid used in the modeling at this level is what
Feynman described as "dry water", every bit as real as those frictionless
and massless pulleys.

Freshman (2nd semester, maybe), Sophomore and Junior years you take more
math like multivariable calculus, linear analysis and applied analysis.
Methods to solve fiendishly complex multivariable differential equations,
partial differential equations. I reached my own level of incompetence in
math with a class in Complex Analysis where math really does diverge from
Reality. Powerful stuff, nearly indistinguishable from magic.

Late in the game, someone actually majoring in physics would take a class in
Mechanics and another in Statistical and Thermal Physics. If engineering,
Fluid Dynamics, maybe a course studying Compressible Flow afterwards. In
these classes (I took the physics route) you start dealing seriously with
different ways of doing that same old Newtonian physics but this time in
much more general terms and with mathematical tools which allow a different
sort of more powerful physical modeling. Let me quote from the introduction
of the text "Mechanics" by Symon:

"A great many of the applications of classical mechanics may be based
directly on Newton's laws of motion. ... There are, however, a number of
other ways of formulating the principles of classical mechanics. The
equations of Lagrange and Hamilton are examples. THEY ARE NOT NEW PHYSICAL
THEORIES [my caps], for they may be derived from Newton's laws, but they are
different ways of expressing the same physical theory. They use more
advanced mathematical concepts, they are in some respects more elegant than
Newton's formulation, and they are in some cases more powerful in that they
allow the solutions of some problems whose solution based directly on
Newton's laws would be very difficult."

Newton's Principia was first published in 1686. In 1687, James Bernoulli,
father of Daniel (the eventual author, in the 1730's, of Hydrodynamica and
the Bernoulli who is most often remembered) was appointed chair of a math
department at a university in Switzerland. James was a noted mathematician
who was a very early proponent of the new calculus. Skip forward, and the
great mathematician and physicist Leonhard Euler, a friend of Daniel's, was
the son of one of James's students, and studied mathematics under James'
brother younger brother John Bernoulli. The forefront of physics and math
were concentrated in a few centers in the 18th century, and these guys were
at the center of it as were the aforementioned Lagrange and Hamilton. Rather
than writing equations of motion directly in the style of Newton, the
Hamilton, Bernoulli and Lagrange equations were derived from the calculus
and Newton's principles of conservation of energy and momentum. Equations of
motions of fluid particles by their positions were first developed by Euler
and are the so-called "Lagrangian equations" of fluid mechanics. The
equations of motion of a moving fluid in terms of density and velocity at
each location are sometimes referred to as the "Eulerian equations"; the
derivation of Bernoulli's equations involve the energy of a moving fluid
using these. Very interesting, powerful stuff, but the basic physics is
exactly the physics of Newton. No new principles, just new and potentially
more powerful tools to use for further study and application.

Let me restate the above: there is no Bernoulli Theory that generates lift
in a way counter to Newton's F=mA. What Bernoulli did in his day (along with
many others) is essentially to take Newton's axioms of physics and the
calculus and apply them in very beautiful, insightful and innovative ways.
Bernoulli saw far because he stood on the shoulders of giants, as did
Newton.

However, none of these tools are useful for kids and pilots who are
interested in the principles that keep airplanes up in the air. Yes,
Bernoulli's insights can model the pressures above and below a wing and the
lift. It still boils down to a Newtonian "the wing generates lift up because
a lot of air is moved down". Why not keep it simple? Proper, efficient
airfoils and barn doors will generate lift at speed if at a proper and
positive angle of attack to move the air down. Airfoils have much better
low speed handling characteristics and less drag at cruise than barn doors,
but angle of attack remains the critical concept that pilots must be aware
of.

Langewische was right. The wing of an airplane in flight bats the air down.
Using this requires at most a very basic knowlege of 17th century physics
and perhaps 11th century algebra. Leave the 18th century physics and the
newer stuff to the specialists.

-Greg

PS A close relation (he was a CFI and ATP in a past life, before he started
flying satellites for a living) has a real aeronautical engineering degree,
and I did have enough of a clue to run the above by him before posting
today. If you want more, keep reading. He added,

"That's a good emphasis on the point that Bernoulli's equation is simply an
energy equation and is ultimately based on Newtonian formulations in the
first place. And the fact that Bernoulli's equation is used with the
assumption that the flow is 'steady and incompressible'. To go a little
further, it also assumes inviscid and irrotational flow - of which, air is
neither. Which leads to the question - why mention Bernoulli in the first
place?

And the answer is, because you use other boundary conditions and flow models
to overlay (superpose) real fluid conditions on the flow so that you can
then pull out the Bernoulli equation to solve for the pressure distribution.
And in so doing, you mask the reality that - as you said - the wing is
turning a mass of air downward to create the resultant lift force on the
wing. At which point, you remember that F=MA is a VECTOR equation with a
little arrow over the F and the A.

So in essence I agree with you, although I think you gave them too much
history. They don't deserve it.

The standard method prior to computer solution of the Navier-Stokes
equations went like this:
1. Assume an inviscid, irrotational flow (Air is neither, but we'll work
that out..)

2. Assume a potential flow, centered at the aerodynamic center of the wing,
that creates a 'vortex flow' about the wing in a clockwise direction.

3. Impose a boundary condition at the trailing edge that requires the
trailing edge upper and lower flow directions to be parallel, and of the
same magnitude.

4. Assert that a 'starting vortex' of opposite sense to the main vortex is
shed by the wing to establish Condition 3. This starting vortex never dies
off in the inviscid formulation. It remains where it originally was in
space, enforcing the irrotationality of the flow which is disrupted by the
assertion of Condition 3 (commonly known as the 'Kutta condition').

5. Now superpose flows 1. and 2., impose Condition 3, include assumption 4,
and calculate the velocity potential wherever you want. Use this velocity
with Bernoulli's to calculate the pressure.

Simple, huh? And real physically intuitive. [he also is more sarcastic than
I am]. It's just a bunch of ROT designed to model a flow in a way that an
ordinary human can calculate it.

The reason a 'vortex' is assumed is to IMPOSE the downward flow seen behind
the wing - to visualize this, add a circulatory flow to a linear flow and,
at arbitrary points ...
 
Go on to college to study more science and you get more of the above your freshman year. Including more massless and frictionless pulleys. Digging out my old Halliday & Resnick "Physics", there were about 650 pages devoted to 25 chapters that I think were covered in the first year. "Bernoulli's equation" is presented in chapter 18 but only in a simplified form that assumes steady and incompressible flow. Chapter 18 (22 pages) is an introduction to fluid dynamics, but it's mostly very basic stuff devoid of calculus, in part because none of the frosh involved had yet taken any
significant multivariable calculus, or how to actually make any sense of
difficult differential equations (or diffyQ's as we'd call them),
multivariable or not. The fluid used in the modeling at this level is what
Feynman described as "dry water", every bit as real as those frictionless
and massless pulleys.

Now, there's a blast from the past. Funny, we keep calling it Halliday and Resnick, but my copy puts Resnick's name first. The scary thing is, while I first used this in the spring of 1971, all I had to do to get it for this message was move a couple of items away from the front of it on the book shelf in my office at home.

Oh, and Bernoulli is introduced in section 18-4 on page 445 of my copyright 1966 copy. :D
 
Hey thanks for that Dave. You just summarized the last 4 yrs of my life.

Im a firm believer that wings only generate lift because pilots tell them too. A firm understanding of AoA is about all a pilot needs to successfully operate a wing. leave the math to the dorks with calculators.
 
This caused a more in depth discussion of lift on another board. Here is one response that discusses Bernoulli in depth, but pretty well says it's much better to keep it simple for most pilots <g>

Let me know if you'd like to see the rest of the post.

Best,

Dave

es, I can hear the groans out there. First, please, if you reply to this
(and it's OK not to), remember to trim it down before posting.
I come to praise Bernoulli, not to bury him, his dad or his uncle. In the
periodic Bernoulli lift debates on rec.aviation.<pick your favorite> there
is always a great deal of heat generated. Personally, I believe that most
schoolkids (and pilots) are best served by a pure Newtonian description of
air being forced downward (and lots of it) instead of a discussion of
differential pressures and Bernoulli, and I'd like to briefly describe why
in a qualitative and historical way. In short, it's because most of you guys
aren't ready for it and I think it hinders, not helps, the understanding of
what is going on. And, I should mention, I am also not competent to apply
Bernoulli's equations to *any* real system today, either. It is not a tool I
use, and I also make no claim to understand the nuances of lift of a real
wing in real air.

<snip snip snip>

So in essence I agree with you, although I think you gave them too much
history. They don't deserve it.

The standard method prior to computer solution of the Navier-Stokes
equations went like this:
1. Assume an inviscid, irrotational flow (Air is neither, but we'll work
that out..)

2. Assume a potential flow, centered at the aerodynamic center of the wing,
that creates a 'vortex flow' about the wing in a clockwise direction.

3. Impose a boundary condition at the trailing edge that requires the
trailing edge upper and lower flow directions to be parallel, and of the
same magnitude.

4. Assert that a 'starting vortex' of opposite sense to the main vortex is
shed by the wing to establish Condition 3. This starting vortex never dies
off in the inviscid formulation. It remains where it originally was in
space, enforcing the irrotationality of the flow which is disrupted by the
assertion of Condition 3 (commonly known as the 'Kutta condition').

5. Now superpose flows 1. and 2., impose Condition 3, include assumption 4,
and calculate the velocity potential wherever you want. Use this velocity
with Bernoulli's to calculate the pressure.

Simple, huh? And real physically intuitive. [he also is more sarcastic than
I am]. It's just a bunch of ROT designed to model a flow in a way that an
ordinary human can calculate it.

The reason a 'vortex' is assumed is to IMPOSE the downward flow seen behind
the wing - to visualize this, add a circulatory flow to a linear flow and,
at arbitrary points ...

Whoa Dave.... be careful with that keyboard will ya... jeeez, I musta hit my head when I passed out somewhere there in the middle of that post, musta forgot to breathe or something. Thank fully there's the summary too!

Now I can't remember why airfoils with increased camber on the upper surface generally generate more lift and drag...
 
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Im a firm believer that wings only generate lift because pilots tell them too. A firm understanding of AoA is about all a pilot needs to successfully operate a wing. leave the math to the dorks with calculators.

I thought according to our friends from England, planes fly based on theory, and if we lose that theory that planes will just fall out of the sky? ;)

I agree, Tony, it comes down to AoA. Dorks with calculators (I think we both fall into the category) will figure out the actual math of it.
 
I agree, Tony, it comes down to AoA. Dorks with calculators (I think we both fall into the category) will figure out the actual math of it.
Haha. I think whoever wrote this...
Why not keep it simple? Proper, efficient
airfoils and barn doors will generate lift at speed if at a proper and
positive angle of attack to move the air down. Airfoils have much better
low speed handling characteristics and less drag at cruise than barn doors,
but angle of attack remains the critical concept that pilots must be aware
of.
...has the right idea.

But some people are really into the theoretical "why" of things. I'm not one of those people. When I study systems I want to see the diagrams on the schematic level, not the engineering level, and the quickest way to get me to close a book is to show me an equation with squiggly symbols.
 
No math, no math, no math... I hate math!

Now, please excuse me while I figure out how long it will take to fly to this station.
 
A firm understanding of AoA is about all a pilot needs to successfully operate a wing. leave the math to the dorks with calculators.
Hey! What about us old dorks with slide rules?

(other than that, you do have a good point - but I still get annoyed with all the mis-information floating around).
 
Hey thanks for that Dave. You just summarized the last 4 yrs of my life.

Im a firm believer that wings only generate lift because pilots tell them too. A firm understanding of AoA is about all a pilot needs to successfully operate a wing. leave the math to the dorks with calculators.

Tony Aren't you supposed to be one of them "Dorks with a Calculator"???
 
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