Determination of the characteristics of tapered wings (1937)
NASA Technical Reports Server (NTRS) · leaf 13
REPORT NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS … 1.4 /£ Angle of attack, a (degreesJ referred to roof chord Lift coefficient CL Cm„-MbfQS* Fioubi 13.-Tapered N. A. C. A. 24-0-0 airfoil. .026 r $3,022 i 9.020 2.2 .44 2.0 .40 0f8 1.8 36 .y %.0/4 1.6 .32 ^8 28 L4 24 ? o/o 20 20*^.008 /6 ■ 16 £ *006 i ^ .52 o 12 O.004 8 &002 A .08 v. o 4 .2 .04 0 0 -…
NASA Technical Reports Server (NTRS)
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