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 NACA slot lip [aileron]
SLUB | 1935
|Experiments on airfoils with aileron and slot
Engineering Index Backfile | 1927
|Full-scale tests of new type N.A.C.A. nose-slot cowling
Engineering Index Backfile | 1937
|Full-scale tests of new type N.A.C.A. nose-slot cowling
Engineering Index Backfile | 1937
|Full-scale tests of new type N.A.C.A. nose-slot cowling
Engineering Index Backfile | 1937
|