Tests made in 7- by 10-ft wind tunnel with 4-by 8-ft wing hinged at tunnel jet boundary and restrained in roll by elastic cords; time histories were taken of motion of control device under test and resulting wing motion.
Development of N.A.C.A. Slot-lip aileron
Nat Advisory Committee Aeronautics -- Tech Notes
1935
10 pages
19 Supp plates
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Development of the N.A.C.A. slot-lip aileron
| TIBKAT | 1935
Development of the NACA slot-lip aileron
| NTRS | 1935
Development of the NACA slot lip [aileron]
| SLUB | 1935
Experiments on airfoils with aileron and slot
| Engineering Index Backfile | 1927
| Engineering Index Backfile | 1934