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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REPORT No. 678 INTERFERENCE OF TAIL SURFACES AND WING AND FUSELAGE FROM TESTS OF 17 COMBINATIONS IN THE N. A. C. A. VARIABLE-DENSITY TUNNEL By Albert Sherman C. A. 0009 section at the tip. It was combined with SUMMARY the fuselage in the standard longitudinal position. An investigation of the… … Figure 1.—Combination 311 showing elliptical tail surfaces. reference 1; it is a duralumin model having an area of d/c=0. The fuselage is the round fuselage described 150 square inches, aspect ratio 6, taper ratio 2, and in reference 1; it is an airship form having a length of the N. A. C. A. 0018…
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