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
301 PRACTICAL METHODS FOB CALCUIATION OF HOEIZONTAL TAIL AEBA The second equation k c = i^,(3 4-0.25 (£)~ ^^"] ^^^^ 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 this condition. Experience indicates, however, that when this adequate restoring moment at zero lift…
NASA Technical Reports Server (NTRS)
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