Wind-tunnel tests of a Clark Y wing with 'Maxwell' leading-edge slots (1937)
NASA Technical Reports Server (NTRS) · leaf 14
I.A.O.A. Teohnloal Vote Ho. 398 Tig.6% t Figure 6 (a).- The Olarlc T wing vita 0.176 o_ Maxwell slat both open and olosed and 0.311 ow split flap both neutfal and defleoted.
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