Span load distribution for tapered wings with partial-span flaps (1937)
NASA Technical Reports Server (NTRS) · leaf 5
to C* «• ct- P 11 313 i-g -3 Section normal-force coefficient and c, 1—« 5" o o \h pr* … o s Incremont of lift coefficient, A CL (\*>0.25) J CD C P o fo Oj Co O f\) o P a o en to §> o o Si + o i > I 1 C*) I—51 il cj i—( >«: "Si s 1 3 I Co Q Cj r\j Co ct> increment of lift coefficient, A Cz (X"I.OJ
NASA Technical Reports Server (NTRS)
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