Preliminary investigation of rolling moments obtained with spoilers on both slotted and plain wings (1932)
NASA Technical Reports Server (NTRS) · leaf 17
N.A.C.A.. Teclmical Note Ko.415 Clark Y wing with, low-drag fixed tip slot 40 per cent of semlepan. Curved spoiler with gap 33 per cent of spoiler height. … Spoiler angle to wing upper surface,6_ (26^ c "back:) Jig.6 Spoiler with gap 33 percent of spoiler height on slotted wing. Clarlc Y wing with low-drsg fixed tip slot 40 percent of seanispan. Curved spoiler with gap 10 per cent of spoiler lieight. —ruT^ .7". -3.0"- JL_ T7- Moujiting flap.-' ^Tapered…
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
