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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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An illustration from Interference of Tail Surfaces and Wing and Fuselage from Tests of 17 Combinations in the N.A.C.A. Variable-Density Tunnel, 1939, leaf 28 — > o > … Lift coefficient CL Lift coefficient, CL Figure 10. Figure 9. to in CD

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