Figs.l,S,3;4,5 N.A.C.A, Technical Memorandum No.493 Fig. 1 … 0.95 0.4 Fuselage. 0.6 0.75 i=5.5 2=2.5 0.45 0.8 rl d Fig. 3 U 50 u u _2=f(r) lOOrl. 120 U dS dr 80 Detached propeller &s 40 dr Propeller at nose 0 of fuse- lage . 4 .6 .8 1.0 m-^r Fig.4 Fig. 5
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
