Analysis of box wing by rational methods results in computation of much lower stresses in various members of box than are obtained when present design procedure is followed; method of least work; Burgess' method of load division; membrane analogy method.
Torsion in box wings
Nat. Advisory Committee Aeronautics -- Tech. Note
1931
44 pages
3 Figs.
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
NTRS | 1931
|SLUB | 1931
|Stressed-Skin Wings in Pure Torsion
Emerald Group Publishing | 1945
|Stresses and deformation in wings subjected to torsion
TIBKAT | 1952
|Stresses and deformations in wings subjected to torsion
NTRS | 1952
|