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
naca-tn-1646
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.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1948/naca-tn-1646.pdf