I don't have time to provide a full response, but I'll hit the major points Steve mentioned.

Addressing my summary where I say Bernoulli does not keep a wing in the air. I am standing by this as I have done the actual experiment proposed at teh end of you last post. If you mesure the pressure differential above and below an airfoil as well as the velocity and plug the data into Bernoulli, it just doesn't cut it. Unfortuantly I have thrown away my report on teh subject from when I was running airfoil tests in a wind tunnel. I do remember though, I used a section of wing from a Cessna 172. I remember the portion of lift attributed to Bernoulli being less than 10%, but I do not remember exactly how much.

Also, you stated the four requirements for being able to use Bernoulli in you post. If you look at a wing in the real world none of the requirements you posted are met. The only one close is the steady flow requirement, but all airfoils have separation before the trailing edge. Therefore you would have to isolate only the portion of the wing that does not have spearation.

I will have more on Coanda later. I have to get back to work.