Inside Out Library · Explore
Tests in the Variable-Density Tunnel of Seven Tapered Wings Having N.A.C.A. 230 Mean Lines, Special Report (1937)
NASA Technical Reports Server (NTRS) · leaf 12
2 .4 .6 .8 1.0 1.2 1.4 1.6 1.8 8 12' 16 20 24 28 32 -4 -.2 ■8-4 0 4 Lift coefficient CL Angle of oflack, oc (degrees) Figure 5.- Tapered N.A.C.A. 5-10-18 airfoil.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
More pictures from Tests in the Variable-Density Tunnel of Seven Tapered Wings Having N.A.C.A. 230 Mean Lines, Special Report
More like this
