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The effects of partial-span plain flaps on the aerodynamic characteristics of a rectangular and a tapered Clark Y wing (1938)
NASA Technical Reports Server (NTRS) · leaf 12
riBi.7,i3 .iO.i. Teobnloal Iota So. 863 O Tip-aaotlon flapi. A Oenter-seotion flap. 13 10 … 0 20 40 60 SO 0 30 40 60 80 100 flap span, pexoent wing epaa. Flap a?aa^ percent wing spaa. Figure 7 - Iff set of flap length on Oi^^n Ojj Figure 13.- Effeot of flap length on OL^.on On a* °Wx.and °n 1/D »* Otmuf at Ol^.and oa L/D at Ol^. Rectangular Clark Y wing. 6f» 60°. Tapered Olark Y wing,…NASA Technical Reports Server (NTRS)
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