Two practical methods for the calculation of the horizontal tail area necessary for a statically stable airplane (1929)
NASA Technical Reports Server (NTRS) · leaf 6
1.12 %!.04 1.00 36 .92. .22 £4 .18 .20 .14 .16 .12 .10 m .08 _ G Gap Raffo, ~ h, Longer span Fig. 3.—Span factors for biplanes Trith nings of eqaal chord equal chords and equal aspect ratios, respectively. These data are based on the theoretical interference values given by Prandtl in N. A. C. A.… … Fig. 4.—Span factors for biplanes wltt wings of equal aspect ratio The effective aspect ratios of the wings and tail having been determiaed, the nest step is dC to find the value of at some given aspect ratio for the wing and tail sections. This value, if not given in Table II, may be obtained from…
NASA Technical Reports Server (NTRS)
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