The lift distribution of wings with end plates (1938)
NASA Technical Reports Server (NTRS) · leaf 20
N.A.C.A. Technical Memorandum No. 856 Figs. 12,13,14,15 … 0.1 0,1 0,3 OA 0,5 O.B Figure 14.- Ratio c80/ce against height and position of end plate. Figure 15.- Theory compared with Schrenk's measurements. '1
NASA Technical Reports Server (NTRS)
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