Downwash measurements behind wings with detached float (1931)
NASA Technical Reports Server (NTRS) · leaf 11
N.A.C.A. Technical Memorandum No. 632 3Pig:10 a = 2U° a = 60° … 0 1.0 0 1.0 0 1.0 0 1.0 p/% p/ lo of symmetry of wing. Fig.10, Pressure distribution in plane Tapered wing.
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
