Two practical methods for the calculation of the horizontal tail area necessary for a statically stable airplane (1929)
NASA Technical Reports Server (NTRS) · leaf 8
PKACTICAL METHODS FOE CALCUIiATIGN OF HOEIZONTAL TAIL- ABEA 297 … Effecfive aspsci raito of wings Fia. 6.—Downwash factor, F: NOTi.—This chart is based on F-l.OO (se« eq. 15). If the fafl location is either high or low a correction moat be applied (see Fig. 5). WING SECTION STABILITr FACTOE Fi The wing section stability factor Jfj =^<7p+o:o is obtained by…
NASA Technical Reports Server (NTRS)
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