Experiments with a wing from which the boundary layer is removed by pressure or suction (1928)
NASA Technical Reports Server (NTRS) · leaf 17
N.A.C.A. Technical Memorandum No.472 Figs.5,6 … 012345678 m/s,v Fig.5 Graphic representation of the values given in Table 1. -w=72 m/s •w= 0 m/s *5-l. m/s,v Fig.6 Graphic representation of the values given in Table I.
NASA Technical Reports Server (NTRS)
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