• Other sources state that max aero benefit of a superduper airfoil vs a cylinder of the same width is about 1:10...So the above seem a bit generous (1:24)

    Both statements can be true, if the Cervelo graph is for an infinitely long tube with its axis at right angles to a homogeneous flow field and the "other source" is for a finite tube raked at bicycle tube angles in the practical bicycle flow field. The actual section of a circular down tube along the flow line is more like the ellipse represented by the second bar on Cervelo's graph.

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