Determination of the characteristics of tapered wings (1937)
NASA Technical Reports Server (NTRS) · leaf 15
REPORT NATIONAL ADVISORY COMMITTEE FOR AERONAUTIC S . -8 -4 0 4 8 /2 /6 20 24 28 32 J O .2 A £ .8 1.0 1.2 1.4 /.6 Angle of attack, a (degrees) referred to root chord * Lift coefficient, CL Ftguhi 17.-Tapered N. A. C. A. 2RH*-«.» airfoil. … 16 '12 -8 -4 0 4 8 /2 16 20 24 28 32 | -.2 0 Lift coefficient, ft Angle of attach, a {degree*), refer red to root chord Fioims IS.—Tapered N. A. C. A. 2Ri-15-0 airfoil.
NASA Technical Reports Server (NTRS)
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