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I’m thinking in a flight controllable prop, but if fitted with the appropriate control system it could be made an automatic constant speed prop.

I didn’t mention than I’m planning to make the prop variable in pitch, so I think that this solve the issue of adapting the prop for the changing conditions, hence than I m not sure about what is the correct chords distribution for this kind of prop. Of course if it were to be fixed pitch you...

Hi, I’ve been trying to design a propeller from cero, I’ve studied Theodorsen´s paper and I do understand the procedure for obtaining the optimum distributions for an specific flying condition (speed, HP, rpm), but how to design the propeller for the whole aircraft operation , because the paper...