Citabria, I admittedly don't know much about stall characteristics.
Why should the F6F-5 have a soft stall?
I'm not asking for people to post up anecdotal comments on how XXX pilot thought the plane was a dream, and it had an easy stall (you can find similar comments from some pilot for just about every plane type ever made in some regard).
But in regards to its actual design, why should that aircraft have a softer stall than it currently has? Honest question.
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Vermillion
**MOL**, Men of Leisure