The aerodynamic characteristics of eight very thick airfoils from tests in the variable density wind tunnel (1932)
NASA Technical Reports Server (NTRS) · leaf 9
654 EEPOKT NATIONAL ADnsOEY COMMITTEE FOR AERONAUTICS 1.2 CI « « - a. FiouBE 16.—N. A. C. A. 6S31 airfoil. From tests In open-tbnmt tunnel -/e -8 o -te ...-B 0 -IB -8 .0.-16' 0-ie -a a 8 16 g4. 32 ce of Of of oe FiGUBE 17.—N. A. C. A. lOS aliton, Ftom tests In open-tbroat tunnd FlsuBE 18.—U. 8. N.… … FioxjBE 19.—N. A. 0. A. 1(H aitfolL From tests In opftn-throat-tunnel
NASA Technical Reports Server (NTRS)
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