Reduction of lift of a wing due to its drag (1935)
NASA Technical Reports Server (NTRS) · leaf 6
U.A,C.A. Technical Memorandum So, 781 Figs 0 ,04 .08 .12 .16 Figure l.~ Laminar friction layer?directional field, x= development of profile, r)~ criterion of friction layer thickness (iv - ^2 * ^) * The figures denote the directions of (d-q/dx). … 6 I L.—i I L 0 .04 .08 .12 .16 Figure 2,- Location of transition point from laminar to turbulent flow, suction side.
NASA Technical Reports Server (NTRS)
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