Propeller design IV : a simple method for determining the strength of propellers (1926)
NASA Technical Reports Server (NTRS) · leaf 17
N.A.C.A. Technical Koto No.238 Fig.6 «-Max. c amb e r = 1.0 Leading j l^f edge '—1 in IS C( « • Blade width"(b) Navy standard blade section. R.A.F.No.6 modified, flat face. … Double carreer Area of upper section = .74 bh-j " lorer " = .74 bhL .UShrjX. 74bhrj».4-l<3hT x . 74bhr ;74biiTj+.74"bh£ ~ = -;416(hL) Fig.6 e.g.and area of sections.
NASA Technical Reports Server (NTRS)
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