Determination of the characteristics of tapered wings (1937)
NASA Technical Reports Server (NTRS) · leaf 14
DETEEMINAT10N OF THE CHARACTERISTICS OP TAPERED WINGS … Lift coefficient CL FiOUTtt 15.-Tapered N. A. C. A. 2*-30-0 airfoil. -16 -12 -8 -4 0 4 8 /2 16 20 24 28 32 2 .4 .6 .8 l.O 1.2 Ang/e of attack. <* (degrees) referred to root chord Lift coefficient CL Figure 16 —Tapered N. A. C. A. 24-3&-8.50airfoil.
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