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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000. The and on the mean chord of f) inches. The methods for testing procedure and the test precision were about the analysis of the test data and for presentation of the same as for au airfoil (reference 8). The three-com- test results are explained in reference 1. ponent balance of the… … Lift coefficient CL Lift coefficient, CL Figure 6.—Effects of tail setting on the characteristics of high-wing combinations. Figure 5— Characteristics of midwing combinations with various tail surfaces. Tapered N. A. C. A. 0018-09 airfoil and round fuselage; /r/c=0.22; ilc=0°. Tapered N. A. 0. A.…
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