Rough guide for conventional configurations:
0.3< ((astabXmomentofstab)/(awingXavgwingchord))<0.6
the number should be bigger if you have more pitching moment and smaller
if you have less, so probably a bit on the large side if you have flaps
astab is, of course, area of stab
awing is same for
I'm would like to build a 2 meter with 600 sq inchs in the wing.
How do I know how much stab area I need? My fuse is a designed for a
flying stab.
David
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