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Determination of the air forces and moments produced by the ailerons of an airplane (1928)
NASA Technical Reports Server (NTRS) · leaf 18
N.A.C.A. Technical Memorandum iJo.483 Figs.5,6,7. .12 0 .2 .4 .6 .8 1.0 21/b Fig.5 Coefficient £ of rolling moment. … 1.0 21/b Fig.6 Coefficient r\ of additional induced drag for opposite aileron settings. ,12r .2 .4 .6 .8 1.0 21/b- Fig.7 Coefficients i of yawing moment.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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