The experimental and calculated characteristics of 22 tapered wings (1938)
NASA Technical Reports Server (NTRS) · leaf 15
REPORT NO. 027—NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS … Angle of attack, of (degrees) referred to roof chord Lift coefficient, CL Figure 19.-Tapere<l N. A. C. A. 23013 43010 airfoil. .026 024 CD ^.022 u.020 ,44 ^.0/8 - 2.2 %.oie 2.0 .40 - 18 .36 ^.0/4 o o .32 1.6 .012 .28^.010 - 1.4 .<» ^ 1.2 .24^.008 Co /.Of .20% ^.006 £ ° * .8 to .16 ^%.004 ■6^./2…
NASA Technical Reports Server (NTRS)
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