Construction of Fowler wing which is fully extended for taking off and at reasonable altitude is drawn in, thus reducing air resistance and increasing speed; for landing it is extended while flying and lands with lower angle of attack; fullscale and wind-tunnel tests of aerodynamic properties; lateral control secured at stall; ability of wing to carry increased pay load. (See also Aviation vol. 25, no. 4, July 21, 1928 pp. 263, 285-286, 3 figs)
The fowler variable area wing
Aero Digest
Aero Digest ; 13 , n 2
1928
2 Figs.
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1928
|Wind-tunnel tests of fowler variable-area wing
Engineering Index Backfile | 1932
|Wind-tunnel Tests of the Fowler Variable-area Wing
NTRS | 1932
|Wind tunnel tests of the fowler variable area wing
SLUB | 1932
|Emerald Group Publishing | 1936
|