Figs. 5,5,7 H.A.C.A. Technical Meaioraadiuri l)To.7l3 1/2 5=, … Figure 5.-Development of area of ?i^ire 6.-Part of area of discorLtinoity Tjeliiad discontiriMity and an airplane wing. circle ovor vrhich it is iis- triljuted after develojaneat. 1.0 0.8 0.6 0.4 0.2 0.2 0.4 0.3 0.3 2r/l a, d(r2TT) 20r^ Figure ?.-Relationship tetv/esn de- liffxre 8.-Flow past…
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