Raskin about how plane wings lift
karmak.org
karmak.org
Wings works the way they do because othey curve the path of the air that flows around them. They deflect the air flow, thus creating a force. http://amasci.com/wing/airgif2.html
The "coanda effect" breaks if you give your lifting surface too high an angle of attack (stall), but a reduced quantity of lift is still produced.
Planes can fly upside down because the increase the angle of attack, and the path the air takes IS longer on the top (flat surface) then it is at the bottom (curved surface). A plane with assymetrical wing section flown upside down at a zero angle of attack will go down. This is why aerobatic planes always use symetrical wing sections.
Flat wings work very poorly and stall at very low angles of attack, beause of flow separation, but they do create lift, because the point where the flow separates between upper and lower surface is not at the leading, but somewhere on the lower surface. See this image: http://www.arvelgentry.com/images/plate2.jpg
This guy should read "Theory of Wing Sections", by Abbbott and Van Doenhoff (http://www.amazon.co.uk/Theory-Sections-Dover-Books-Physics/...) before posting misleading essays.
Sorry about the rant, but I don't want anyone taking what this guy writes for the absolute truth...
Obligatory xkcd reference: http://xkcd.com/386/
He then goes on to talk about the Coanda effect, and how that combined with the shape of the wing makes the wing direct air toward the ground, and thus provides lift.
Suppose back in sixth grade, his teacher had taught that explanation instead of the incorrect Bernoulli effect explanation. He'd still have the same problem! Turn a wing upside down and the Coanda effect and shape are now deflecting air toward the sky, and the lift is toward the ground.
He should have had a little section at the end covering how planes actually fly upside down.
There are at least four ways to force air downward in order to help provide lift. There's the Bernoulli effect, which he points out doesn't provide very much lift. There's the Coanda effect, which he covers. Then there's simple brute force--point whatever you are using to provide thrust so that the thrust vector aims up somewhat instead of level. Finally, put something in the air flow at an angle so that it directly deflects the airflow down.
The first two work in the wrong direction when upside down, so it is the later two that are responsible for upside down flight. Note that both of these come with significant cost. If you are pointing your thrust vector up, you lose some forward thrust, so it is going to take longer and cost more in fuel to get where you are going. If you stick some flat surface in the air flow to just directly direct air downward, you are also introducing considerable drag, again making your trip take longer and use a lot more fuel.
WARNING: the above site can be a HUGE time sink.
Lift is generated due various reasons: I recommend a read here http://en.wikipedia.org/wiki/Lift_(force)#A_more_rigorous_ph....
(Yes, they're both from Wikipedia and I feel a bit ashamed that I couldn't find a better source but the description there is succinct and rather complete -- I can vouch with my Aero Eng degree on the information there! :D).
Flat wings work with a positive angle of attack (EX: paper airplane). The problem with scaling this up is turbulence at the sharp edge. A gently curved surface reduces turbulence and drag. Remove enough turbulence and you get a laminar flow which hugs both sides of the wings. You can deflect a laminar flow down to increase lift. (See faucet experiment.) Control surfaces on the wing redirect the flow to push the aircraft in a new direction. Incresing the angle of attack increases lift until you reach the critical angle of attack ~15 degrees when you lose laminar flow and a sudden drop in lift occurs. Stall speed is the speed below which you can't maintain level flight by increasing angle of attack. High performance aircraft and trade efficiency for performance (EX: an F-15 landed after losing a wing http://www.uss-bennington.org/phz-nowing-f15.html)
Super sonic flight behaves somewhat differently. (See faucet with increased pressure.)
Nonsense. Everything is wrong until proven otherwise. The burden is on the presenter to justify the statement. The moment doubt is raised then the presenter must address it. Someone pointing out a logical error in the presenter's assertion is not required to come up with some other explanation in order to explain that error.
Of course if they do they are held to the same standard.
There are many crackpots that 'have been shocked to realize that library books and teachers were wrong and that they should trust their own thinking in the face of concerted opposition'. Only slightly different from the original, but the italicized words make a world of difference. Einstein's (special) theory of relativity faces scores of opponents that 'trust their own thinking', despite not having a single fact that casts doubt on it.
But indeed, even the aerodynamics manuals we were given simplified this part quite a bit.
http://www.ted.com/index.php/talks/jonathan_drori_on_what_we...
Was completely blown away, and angry at my education. And at myself for believing it so easily.
A question I always had about the circulation vortex: where's the energy input to power the vortex?! (or why does it not need one?)
To be less facetious, the energy input is the moving airfoil at a particular angle of attack.
http://www.av8n.com/how/htm/airfoils.html#sec-airfoils-summa...
My question: why/how does the air do this?
For example, I thought the Coanda effect was the macro result of van der Waals attraction. Is there a similar explanation for the behavior of air which results in asymmetric leading & trailing edge behavior?
Can anybody please explain that, or link to an explanation?
I'm blown away by how many sailors believe in the equal transit theory.
As Rodney Brooks said: "The world is its own best model"
Bernoulli's principle is basically a statement about what happens when you apply Newton's laws to a macroscopic amount of fluid and allows you to determine what happens when an asymmetrical object is placed in the flow of such a fluid: when the speed goes up, the pressure goes down. Pressure is nothing but the amount of Newtonian action exerted on a surface, which brings us back to the third law.
Then you find that Bernoulli's principle doesn't quite cut it, because it doesn't take into account that fluids don't actually behave like the naive application of Newton's laws would lead you to believe. However, in the end, the Coanda effect is again a description of the behavior of fluids under certain circumstances, describing the macroscopic effect of Newton's laws applied to all individual particles.
[1] The exact difference between the two is subject of much philosophical debate, but most would agree that something like Bernoulli's principle has more explanatory power than Newton's law, because, for instance, it allows you to understand why a wing would lift.
The word "just" covers a lot of detail that can make the short explanation less satisfying--especially if you're trying to use it to build something.