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Bill,
I found your last email somewhat stimulating. I believe that I can shed
some light on the situation. I will first start by giving a quote from
Elementary Fluid Dynamics, by D.J. Acheson, Clarendon Press, Oxford:
Notwithstanding the importance of circulation, the Kutta-Joukowski
condition, and the theorem of [the previous section which relates lift
to speed and circulation], an aerofoil obtains lift essentially by
imparting downward momentum to the oncoming airstream. In the case of
a single aerofoil, in an infinite expanse of fluid this elementary
truth is disguised, perhaps, by the way that the deflection of the
airstream tends to zero at infinity.
There should be no question that the net result of lift is that air is
given vertical momentum and energy. The confusion comes from the 2D
simulations of the aeronautical engineers. I think you will have an
easier time visualizing the 2D situation if you keep in mind that a 2D
airfoil is really an airfoil of infinite length. This fact is often lost
and is the cause of much of the confusion.
It is the loss of the fact that 2D simulations are of infinite wings that
give rise to the (silly) misconceptions that lift does not require work
(the basis for the book Stop Abusing Bernoulli! How Airplanes Really Fly,
By Gail Craig), that if one were to look far enough back there would be no
net momentum transfer,
The point was brought up in the email that many textbooks and expert
cannot possibly be wrong. Through the years of developing the view that
is presented in our paper, many a time I almost quit because of something
that I read from an expert. I would be stopped by the thought that if
what was said were true, that I really didn't know how a wing developed
lift. Fortunately for me, Scott was there to explain the origin of the
misconceptions. This work has been more of an effort in learning where
misconception came from than figuring out how planes really fly.