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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 22
N.A.C.A. Technical Note No.415 Jig.12 Plain Claxk Y wing. Ciirved spoiler 10 per cent chord wide and 40 per cent sanispan long, 5° deflection only. … Hg,12 Effect of spoiler location on rolling~moment coefficient for anall angular deflections. 10 per cent chord spoiler on plain wing.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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