Lift, drag and center of pressure characteristics of model of Fowler variable-area wing measured in N.A.C.A. 7 by 10 ft wind tunnel; highest lift coefficient obtained was 3.17 as compared with 1.27 for main wing alone.
Wind-tunnel tests of fowler variable-area wing
Nat Advisory Committee Aeronautics -- Tech Notes
1932
6 pages
12 Supp plates
Report
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Wind-tunnel Tests of the Fowler Variable-area Wing
NTRS | 1932
|Wind tunnel tests of the fowler variable area wing
SLUB | 1932
|Engineering Index Backfile | 1928
|Engineering Index Backfile | 1928
|