160 REPORr NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS. 7VA Fig. 2.—Dimension of Sloans aerofoil. [All dimensions given. as_d«lmal part of chord.] Offsets (measured from and.Xto^chord). … Pig. 3.—Dimensions of R. A. F. 6 aerofoil. [All dimensions given as decimal part of chord.] , Distance from leading G.&0 400 edge ! Upper camber: .075 I Specified .0763 Actual Lower camber: .0067 ,008 Actual... Offsets (measured from and JL to chord). METHOD OF TEST. During the tests each aerofoil…
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
