Investigation carried out in 5-ft. wind tunnel of Langley Memorial Aeronautical Laboratory for purpose of obtaining more complete information than was heretofore available on distribution of lift between ends of wing spars, stresses in ailerons, and general subject of air flow near tip of wing.
The distribution of lift over wing tips and ailerons
U. S. Nat. Advisory Committee Aeronautics. Report
1923
24 pages
29 Figs.
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
The distribution of lift over wing tips and ailerons
TIBKAT | 1923
|Engineering Index Backfile | 1938
|