Maximum angular accelerations in roll and yaw produced by sudden application of ailerons and maximum accelerations in yaw produced by sudden application of rudder during gliding flight recorded for following wing arrangements: no auxiliary device; full-span slots; plain flaps; flaps and full-span slots.
Effect of slots and flaps on lateral control of low-wing monoplane as determined in flight
Nat Advisory Committee Aeronautics -- Tech Notes
1933
11 pages
12 Supp Sheets
Article (Journal)
English
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Engineering Index Backfile | 1934
|A note on lateral control with a cantilever monoplane wing
Engineering Index Backfile | 1928
|