Interference of Tail Surfaces and Wing and Fuselage from Tests of 17 Combinations in the N.A.C.A. Variable-Density Tunnel (1939)
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2 REPORT NO. 678—NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS 20.156 inches and a fineness ratio of 5.86. The tapered I tion (reference 5). Figures 1,2, and 3 are photographs fillets (reference 1) were carefully constructed of plaster of interesting combinations and show the proportions … Figure 2—Combination 31G showing rectangular tail surfaces with end plates. Figure 4.—Details of the tail surfaces—N. A. C. A. 0009 sections. percent as large. Only very small fillets wnv used at the tail surfaces (see figs. 1 and 2) because filleting was believed unnecessary for the junctures…
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