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 10
.C Tested: L.M.A.L. VeI.(ft/sec): 68.1 Date: 2-7-36 Test: V.D.T. 1332 Corrected for tunnel-wall effect R.N. (Effective): 6,710,000 a, 28 32 .2 .4 .6 .8 1.0 1.2 1.4 1.6 IB -q -4 0 4 8 /2 16 20 24 r4 L ift coefficient, CL Angle of attack, a (degrees) Figure 3.- Tapered N.A.C.A. 3-10-18 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
