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Preliminary investigation of rolling moments obtained with spoilers on both slotted and plain wings (1932)
NASA Technical Reports Server (NTRS) · leaf 25
TS.XiCJL, Tedmical Note No.415 Plain Clark Y wiBg. Spoilers and ailerons deflected individually. O—^ 10^ c "by 60^ Td/2 spoiler up 60° £3 25}^ c "by 4C^ 13/2 ailerons ±25° … 0° 10° 20° 30° 40° Angle of attack,a Fig.15 Conipstrison of spoiler with, average ailerons. Plain wing.NASA Technical Reports Server (NTRS)
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