The standard explaination of the airplane wing involves a pressure difference between the top and bottom. I don't see how the force is on the upper surface rather then the bottom.PaulS wrote: The main resistance provided by the blade near the catch is not off the face of the blade, but off the back of the blade just as off the upper surface of a wing.
Furthermore the standard explaination is overly simplistic: An airplaine wing must actually push air downward. (One can good at decent approximation of lift on a "flat plate wing" just by considering momentum. Newton calculated it before Bernollui)
I've run accross a few good discusions of lift and airplaine wings on the web. If I get a chance to find them I will post a link or excerpt.
Also according to someone I spoke to at CII, the back side of the blade actually has a detached boundary layer.
Its going to take some research and thought before I am satified I understand what is going on. The more I think about it the harder the problem seems.
PaulS wrote: Since you are an experimentalist perhaps this would help...
I twice attempted to to feel the lift with a blade on the dock but not exactly the way you describe. I will try your experiment and hopefully I can get into a double before too long and try that too.
If this goes on, we should proably move this to a seperate thread. Appologies to all who wanted to remain on topic.