NACA Airfoils parameters
NACA Airfoils parameters
(OP)
Hello
Someone can tell me how the NACA parameters are defined? For example if I wanna build a prop how I know the m value(MAX camber) and the p value( Position of Máx camber)of my own prop project?
Someone can tell me how the NACA parameters are defined? For example if I wanna build a prop how I know the m value(MAX camber) and the p value( Position of Máx camber)of my own prop project?





RE: NACA Airfoils parameters
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