Interesting points and very clever of both you and Charlie! So if there is zero or negative slippage, does it mean that the effective pitch used in the calculation is wrong (hard to nail down as Charlie said) or just that the airfoil cross section of the blade is generating thrust at zero slippage? Maybe what I said that slippage cannot be zero (intuitively) would only be true for a symmetrical blade cross section? As you said Tracy it is possible to fly at 0 degree AOA, but this is because it is a non-symmetric wing airfoil cross section, right?
Agreed, I miss the e-mail addresses in the headers. For example, which Tracy? You can't get a clue from the headers anymore...