Tests conducted on three wings with 42° sweepback having aspect ratios of 5.9, 3, and 2, and two wings with 38° sweepforward having aspect ratios of 5.9 and 3; wings of aspect ratio 5.9 were longitudinally unstable at stall but reducing aspect ratio tended to eliminate instability.
Low-speed stability and damping-in-roll characteristics of some highly swept wings
Nat Advisory Committee Aeronautics -- Tech Note
1947
9 pages
12 Supp plates
Report
English
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Engineering Index Backfile | 1947
|Some theoretical low-speed span loading characteristics of swept wings in roll and sideslip
Engineering Index Backfile | 1949
|Some theoretical low-speed span loading characteristics of swept wings in roll and sideslip
Engineering Index Backfile | 1950
|