Does anyone know a straightforward way of applying Riblett's camberline method in Rhino? The NACA camber line approach maps directly to the "flow along curve" tool; but there's no "shear along curve" equivalent.
Alternately, is there a tool which can externally generate these airfoils? I suppose I could write my own, just a bit lazy today. I'm looking for (let's call it) the 230xxR family; that is, the 23000 camber line, with Riblett application to NACA 4-digit thicknesses in the 12% - 30% range.
Alternately, is there a tool which can externally generate these airfoils? I suppose I could write my own, just a bit lazy today. I'm looking for (let's call it) the 230xxR family; that is, the 23000 camber line, with Riblett application to NACA 4-digit thicknesses in the 12% - 30% range.
