Inside Out Library · Explore
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 27
> > … Lift coefficient CL Lift coefficient CL Figure 7. Figure 8. CO boNASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
More pictures from Interference of Tail Surfaces and Wing and Fuselage from Tests of 17 Combinations in the N.A.C.A. Variable-Density Tunnel
More like this