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Tests of three tapered airfoils based on the N.A.C.A. 2200, the N.A.C.A.-M6, and the Clark Y sections (1934)
NASA Technical Reports Server (NTRS) · leaf 9
Root sections ■< 6.000 30 percent •tationa.^ __Jl Figure 1. Dimensions of the airfoil* expretged ae ratioe to ths mean obord.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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