Aerodynamic characteristics of several airfoils of low aspect ratio (1935)
NASA Technical Reports Server (NTRS) · leaf 16
a nel of airfoil of reference 4, refinishec JUL .02 o A o -- 9 o— — O — 1 M f-i B— .01 t3 £5 •H S3 •H 2 Dihedral factor, K 0*3 Figure 5.- Effect of dihedral on maximum lift coefficient and minimum drag coefficient. Circular Clark Y airfoils.
NASA Technical Reports Server (NTRS)
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