Wind-tunnel research comparing lateral control devices, particularly at high angles of attack I : ordinary ailerons on rectangular wings (1933)
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with all three sizes of ailerons with the equal up-and- The highest, strangely, occurred with the long, narrow down deflections, and at the angles of attack just above ailerons having equal up-and-down deflection, al- the stall they are greater than can be obtained with the though these gave the… … appreciable amount of control against 20° sideslip. Fioote 18.—Boiling criterion, 40 per cent e by 30 per cent 6/2 ailerons with various movements Below the stall, all the ailerons have an increased margin of excess control moment as the angle of attack there are still some rather large undesirable…
NASA Technical Reports Server (NTRS)
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