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At the Reynolds numbers at which these things are operating it has been found ... etc ... etc ...
Yes, for this size, flat plate is less complicating than camber, that's experimental rather than mathematical
Set the wing at 2 - 3 degrees and the tail at 0 degrees and don't stray far from that.
Nose (or tail) weight as needed to bring the centre of gravity to about a third of the chord back.
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