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Tests of three tapered airfoils based on the N.A.C.A. 2200, the N.A.C.A.-M6, and the Clark Y sections (1934)
NASA Technical Reports Server (NTRS) · leaf 11
Angle of attack, a (degrees) Size: 5" (mean chord) x 30" Figure 3.- Airfoil: Tapered N.A.C.A. -MB R.N., 3,170,000 Press, (et'n'd'. atm.); 30.6. Dates: 1-7-33, 4-5-33. Vel. {ft./sec.); 69.0 944, 1016, Results corrected for tunnel-wall effeot. Where tested: L.M.A.L. Teste; V.P.T.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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