"Of interest is that the primary problem that George found with the "Chief" was that it "snapped" in hard corners,"
Yep! Tis true!
I 'snapped' the outboard wing off the Chief at KIO this year.
OOPS! Bear in mind they used to build from what we could call medium or hard balsa, not the specially-chosen 4.5 lb superlight stuff we currently seek out. You have to make the spar a lot bigger with 5-lb wood than with 12 lb.
In this case, near as I can tell, the "roll" problem was that the airplane was driven into a stall by excessive pitch rate enabled by the relatively short tail. Lengthening the tail slows the maximum pitch rate, gave it more acceleration to start and stop, allowing (later) larger flaps. How much of this he had thought through, and how much of it was just trial and error, hard to say, but he had to have had some notion because lengthening the tail moment is not at an obvious solution for a roll issue. It's actually quite brilliant compared to a lot of the thinking at the time.
Whenever I asked him about stuff like this, he was a little vague, but I could never tell if it was because he didn't know, or because he didn't want to explain it, was hard to say. He was certainly no dummy, he definitely knew more than he usually let on.
Anyone who hasn't read "Stunting can be smooth" has really missed something, it's as good a piece of engineering reasoning as anyone had done at the time, and you really need to see how far ahead of everybody else he was. Most of it is still relevant today, which is really saying something. The biggest thing that strikes me from is is that he sat down and didn't start with calculating minimum turn radii or reading airfoil polars, he first decided to figure out what he needed to do to get the highest score, and worked from that. I think that's how he avoided the trap that others, like (forgive me) Wild Bill, fell into.
Brett