Results show that wing equipped with group of spoiler segments located near wing trailing edge, slightly inboard from wing tip, and skewed with reference to wing so as to be perpendicular to free stream air flow will exhibit fairly high values of rolling moment throughout usable lift range.
Low-speed wind-tunnel investigation of various plain-spoiler configurations for lateral control on 42° sweptback wing
Nat Advisory Committee Aeronautics -- Tech Note
1948
29 pages
Report
English
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Low-speed wind-tunnel investigation of triangular sweptback air inlet in root of 45° sweptback wing
Engineering Index Backfile | 1955
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