Interference of Tail Surfaces and Wing and Fuselage from Tests of 17 Combinations in the N.A.C.A. Variable-Density Tunnel (1939)
NASA Technical Reports Server (NTRS) · leaf 6
ontain the restricted the study of the vertical tail surfaces to the aerodynamic characteristics of the wing- and of the zero-yaw condition. .2 .4 .6 .8 Lift coefficient CL Lift coefficient, CL Figure 6.—Effects of tail setting on the characteristics of high-wing combinations. Figure 5—… … Lift coefficient, CL Lift coefficient, CL Figure 8.—Effects of wing vertical position. Tapered N. A. C. A. 0018-09 airfoil Figure 7—Effects of tail setting on the characteristics of low-wing combinations. and round fuselage; iu>=0°; i,=0°. Tapered N. A. C. A. 0018-09 airfoil and round fuselage;…
NASA Technical Reports Server (NTRS)
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