The aerodynamic characteristics of eight very thick airfoils from tests in the variable density wind tunnel (1932)
NASA Technical Reports Server (NTRS) · leaf 6
551 TBDB AERODTlfAMIC CHABACTBEISTICS OF AIKFOILS J}9 ^.06 28* 24" OS 04 ' I I- ■03 02 O/ ■8' 4 8 IZ 16 SO 0 .2 .4- .B .6 Ul Angle ofoffack in degrees, a Lift caefffctenf (Absa/ufe), TIOUBX 8.—K. A. C. A. 8321 alrtoll. … iCz/jf coefficieni (Absatuie), Cc Angle of atfactf in degrees, cL FiouBK B.—K. A. C. A. 103 abfolL C^Ia<Kfie<I dosed-tbroat tannel)
NASA Technical Reports Server (NTRS)
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