Determination of the air forces and moments produced by the ailerons of an airplane (1928)
NASA Technical Reports Server (NTRS) · leaf 19
N.A.O.A. Technical Memorandum No.488 Figs.8,9,10. .8 p=4.0 4.5 Fig.8 Coefficients 6.0 * of additional lift for like aileron settings. .8 1.0 1P=4.0 4.5 Fig.9 5,0 Coefficient k of 5.5 additional induced 6.0 drag for like aileron settings. … a
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
