Interference of Wing and Fuselage from Tests of 209 Combinations in the NACA Variable-Density Tunnel (1936)
NASA Technical Reports Server (NTRS) · leaf 6
ing, 3.47 inches P § 5 a <u y outside diameter, was constructed of a single thickness of metal arranged to slip over the engine. For tests .64 25 0 -25 -.75 with the rectangular fuselage the shape of the rear Disp/ocement ofairfoil quarter-chord axis from fuse- lage quarter-chord point in terms of… … of the method of testing is given in reference 13. Figure 2.—A wind-tunnel set-up of a connected wing-fuselage combination. The tests were of two distinct types, one type in which the forces on the wing and fuselage as a unit the tests were the same as those of the usual airfoil were determined,…
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