Two practical methods for the calculation of the horizontal tail area necessary for a statically stable airplane (1929)
NASA Technical Reports Server (NTRS) · leaf 12
^^^ is based on considerations at zero lift, and it merely insures an adequate positive moment for FiQ. 11.—EfEeot of tail aspect ratio on horizontal tall area re- Fio. 12.—Effect of tail lengtli on liorizontal tail area required to quired for constant static stability constant static stability… … '^0 .24 .28 .32 .36 .40 .44 .48 .52 a/c = c. g. focafion off of hading edge of mean wing chord Fic. 13.—Effect of fore and aft c. g. location on horizontal tail area required for constant static stability For a c. g. location at about 30 per e-ent of the mean chord the two equations give almost…
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