Effect of retractable-spoiler location on rolling- and yawing-moment coefficients (1934)
NASA Technical Reports Server (NTRS) · leaf 13
>> * ■ Control arm, y\ ,Control deflected … 100 30 40 50 60 70 Stations,percent chord \ \ Figure 1.- Section of Clark Y wing showing locations of retractable spoilers and a 20 percent c split flap.
NASA Technical Reports Server (NTRS)
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