What the fuck, MIT graduates with problems of lighting a bulb with a wire. FUck.
Damnit, see my last post. The people who couldn't do it aren't from MIT; they're from Harvard! Not that I'm faulting Harvard (though it is nice to poke fun at Harvard...), since none of those students would have been engineers of any kind.
coxmaster: yep, it is commonly taught, but that doesn't make it any more correct. See below...
Minjin: Right but the students they were polling weren't engineering students. They could've been graduates of the divinity program or the business school for all we know. I don't even know what is taught in either of those programs, so I certainly cannot expect their graduates to know anything about engineering... even basic stuff. Which is why I was saying the whole video is completely pointless.
******** weeeeeeeeee time for an epic tangent **********
As for lift... I assume you're referring to something like this:
http://warp.povusers.org/grrr/airfoilmyth.html
That is wrong in so many ways. For starters, Bernoulli's Eqn cannot be used in the way that they're using it when viscosity is a factor. What they have labeled as the "low pressure bubble" coincides with what is called a boundary layer, and the pressure in the boundary layer is the same as the pressure at the edge of the boundary layer (to first order). The boundary layer forms purely as a result of viscosity. The notion of a 'low pressure bubble' is misconceived; it's not like there's a region where the pressure is low, and everywhere else the pressure is high. Also the thing they call 'downwash' is not downwash at all; downwash is the effect responsible for what's called "induced drag."
It's kind of disturbing that even sites claiming to disprove the myth about lift only manage to introduce more errors.
Bernoulli does not play any effect in the generation of lift. At all. I don't need to know *anything* about Bernoulli and I can accurately calculate the amount of lift generated by an object. Like mass and energy, momentum is conserved. So you can draw a box (or a cube) around the wing (or airplane). Now measure the air's momentum coming in, and the air's momentum coming out of the box. The air has experienced some net change in momentum--which we know must be caused by a force*. By newton's third law, the wing or airplane will have experienced the opposing change. The component of this force in the direction of the plane's travel is the drag. The component of the force perpendicular to the plane's travel is the lift. Which is to say, if a plane is traveling "to the left," then the air behind it will have some downward direction (if the plane is generating lift).
The stuff below is more detailed than is really necessary... basically lift is all about momentum changes.
If someone asks you "how does a wing generate lift," you answer "momentum exchange with the atmosphere." The wing pushes on the air. The air pushes on the earth. Action and reaction. It's like jumping on a bed... you push down on the mattress, which in turn pushes on the ground.
Keep reading if you want to watch me try and stumble through a semester of undergraduate fluid mechanics in a few paragraphs, lol.
*Ok, so some of you might be wondering "what about pressure?" I've included pressure (defined as force acting over an area) in the general "force" category. If you count pressure & external forces separately, then depending on how you draw the box, the explanation for lift will be different. Say --- is my wing:
____
| |
| |
| --- |
| |
|___|
A narrow, tall box like that one will tell you that lift is from a change in momentum of the air. A box that is instead wide and short will tell you that lift is from top/bottom pressure differences. A box that's somewhere in between (like a square) will split the difference evenly. This is simply b/c pressure & momentum are intimately related.
Basically, the equation that describes the conservation of momentum goes something like this:
[change in momentum of the air in the box] + [momentum flowing out] - [momentum flowing in] = forces
But "forces" is often broken down into additional components... like force from viscosity (drag), forces from gravity, force from pressure, force from the engines, force from blahblah, etc. So if you let pressure be its own thing, then the only way the air can interact with the wing is through pressure. So you integrate (i.e., sum up) the pressure over every "point" on the surface of the wing, and that's the net force (from pressure) felt by the wing. (In 2D, that's all lift. In 3D, that's lift and a component of drag--this "induced drag" business I mentioned earlier.) Changing the shape of the "box" (called a control volume) changes how you are measuring what the wing feels--whether you're going after the momentum change of the air, or going after the pressure over the whole wing.
So whether you want to call it momentum, pressure, or both is all a matter of accounting. I like momentum b/c it's a nice, simple explanation.
Also, in practice, your box will have a hole in it to make the quantities actually computable... see page 2 here for a picture of what I mean:
http://ocw.mit.edu/courses/aeronaut...2005-spring-2006/fluid-mechanics/f09_fall.pdf