Low-speed wind-tunnel investigation of various plain-spoiler configurations for lateral control on a 42 degree sweptback wing

Leslie E. Schneiter, James M. Watson
Jun 1948

A low-speed wind-tunnel investigation of an exploratory nature has been performed to determine a satisfactory location for a spoiler lateral-control device for a sweptback wing. The semispan wing used for the tests had 42 degree sweepback referred to the wing leading edge and an aspect ratio of 4.01.

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