In the past, other people have plugged in the numbers to java prop and other propeller programs to get static thrust figures, I think spork might have that data for the prop in question from the dynamo tests, but I have never seen it.
I've only run the numbers for beyond wind speed, since that's the only regime the formulas I know can develop useful numbers for thrust vs power. They don't work for speeds of 0 or less through the air.
And how much thrust is generated at 0.1rpm, as the cart begins to move?
The programme does not even produce a result for that AV. All of the math behind that programme is available in the given references, and that
will would tell you why.
A Cessna's engine is not geared to the wheels, such that the forward velocity is directly related to the engine's RPM. There are no planes anywhere, specialist or not, that employ the technique, including aircraft carriers where a short runway is the only option.
The gearing forces the engine to accelerate the prop, and the entire plane at the same time, and laughably in the case of the BB, to drive it the other way.
Gearing to the wheels is not an enhancement, but a naive error, based upon barefoot physics of
literally "screwing props".
The trial conditions, and test procedure are rigged to see that error is not exposed. Replace Jenkins with me, and I would take on 100 zealots, and leave them with a lot to explain. You can be assured of that.
Llyricist is busy trying to deny the established RMS technique, upon the absurd basis that is gives "the bigger number", but does not seem to consider that the simple average may have been inculcated, because it produces the
lowest number.