DiracPool said:
However, I just recently watched a documentary that aimed to debunk this as a myth, saying that there is no air pressure difference since the laminar flow of the wind simply wraps around the wing and meets at the other side.
This is incorrect. If there is a lift force that is generated by the air, it
must be accompanied by a pressure difference. Further, the concept of laminar flow has essentially nothing directly to do with the generation of lift. It can affect the values of lift and drag, but it is not part of the fundamental reason lift exists.
DiracPool said:
The actual cause of the lift, according to this documentary, was simply the force of the wind hitting the bottom of the wing, and that lift was created because planes fly slightly tilted with their pitch upward into the wind which forces the plane upwards. They debunked the pressure differential idea by saying if that were true, then planes wouldn't be able to fly upside-down, which they obviously could do. I thought that was kid of interesting. Unfortunately, I can't remember the name of the documentary.
Well, they are mostly right. You can really look at lift two ways: either through the deflection of the air downward or through the pressure difference created on either side of the airfoil. Both of these can accurately describe the lift generated by a wing and both allow for a plane's ability to fly upside down. The thing that makes many of the pressure different explanations wrong is that they don't explain (or incorrectly explain) why that pressure difference exists (hint: it has nothing to do with "equal transit time"). If done correctly, you could solve for the flow around an airfoil and use the pressure differences to calculate lift and drag
or draw a control volume around it and look at hte net momentum change due to action of the body and you would get the same answer for lift and drag. Both explanations work equally well. The pressure explanation is often a lot easier to use in practice, however.
Which brings me to...
CWatters said:
Before long you will come across groups of people who argue endlessly over two different theories. One group say that lift is caused by the pressure difference above and below the wing. The other group say it's caused by the wing deflecting the air downwards. The real answer is both are correct...
http://www.grc.nasa.gov/WWW/k-12/airplane/bernnew.html
As CWatters alludes to, this causes a downright comical debate between two warring factions who, in essence, are both correct anyway. It is sort of a chicken vs. egg debate.
A.T. said:
What do you guys make of the "New Theory of Flight" by Claes Johnson?
https://www.youtube.com/watch?v=t7e_6bkUFzE
http://secretofflight.wordpress.com/
Is this really something completely new, or just more detail? Does his "elegant separation" apply to stalled wings only, or in general?
This sounds like a bit of over-promoting their own work. They really didn't present anything new in that presentation, and I would even argue that some if it is wrong. For example, saying Kutta-Joukowski does not describe real physics is true by definition, as that theory makes the assumption that the flow is inviscid and incompressible, which obviously doesn't describe the real world. Further, pretty much everyone already knew that you had three major factors affecting lift and drag: vertical pressure differences, horizontal pressure differences and separation (viscosity would be another major contributor as well). I really see nothing new here. Further, I disagree with the idea that a large rounded-edge airfoil will necessarily produce lift. At low angle of attack with no separation, it would not. It requires that separation to prevent the flow from simply remaining symmetric.