Wind-tunnel research comparing lateral control devices, particularly at high angles of attack V : spoilers and ailerons on rectangular wings (1933)
NASA Technical Reports Server (NTRS) · leaf 1
uch a manner as to oppose the aileron hinge the spoiler was down. The various spoilers and moments and reduce the control force required. Hinge ailerons are shown in Figures 1 and 2. moments were measured for the spoiler operating alone Because in the spoiler and aileron combinations the and also… … The results are given as absolute coefficients of the Tiocbe L—Clark Y wing with plain ailerons 25 per cent e by 40 per cent 6/2 forces and moments: and spoiler arrangements various combinations are compared by means of a number of critenons that are being used throughout _ drag •the entire…
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
