Inside Out Library · Explore
The effect of weight and drag on the sinking speed and lift/drag ratio of gliders (1934)
NASA Technical Reports Server (NTRS) · leaf 9
Jig. 2 759 N.A.C.A. Technical Memorandum Fo. 60 emin Aspect, ratio needed -for 40 .... 4J> . v min = 40 Wii IS Structurally possible aspect ratio p, 20 CO vz rain 0 24 16 . 20 12 Span b, m ^■At 50 km/h flight speed (ca= 1) .04 At 30 Icn/h flight speed (ca = 0.4) .02 ,02 .01 0 [S\x\\\^… … 120 + 35(^)1,5 kg; Airplane series: b=12 to 24'm; 0 = Figure 2.- vmin Ca= 1.6 = 40 lan/hNASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
More pictures from The effect of weight and drag on the sinking speed and lift/drag ratio of gliders
More like this
