Model Experiments on the Forces and Moments Acting on an End Plate Fitted to a Wing (1938)
NASA Technical Reports Server (NTRS) · leaf 6
Figs,3,4 N.A.C*A.Technical memorandum No. 85b .4 -air a » 7.0° n « 3.5° m = qo " ■ -3.5° " = -7.0° -.2 -.4 ~.0<± 0 .04 .08 cwF -.1 0 .1 .2 CmF Figure 3.- Polar and moment curve of the wing. … Figure 4.- Coefficients of siie force csF against angle of sideslip V (for designation of y and CBf see fig, 1 )
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