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Forces and moments on a yawed airfoil (1939)
NASA Technical Reports Server (NTRS) · leaf 17
Figs. 2,8 N.A.C.A. Technical Memorandum No.. 906 +■ Blank(4) rectangle ca=1.36 y « X = 5 Ca= .62 13 tf.A.C.A. (6) rectangle A =6 … 0 4 8 12 Angle of dihedral, <p ,deg. Figure 2.- Supplementary lateral force due to dihedral. .00020 3cNv/d°a 3(t*>)° .00010 1.2 .4 .8 0 l/A. = F/o2 Figure 8.- Additional yawing-rolling moments caused by dihedral.NASA Technical Reports Server (NTRS)
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