Method combines theory of elasticity with technique of succesive approximations; it can be employed by calculators with little previous training, and converges rapidly to exact solution. (See also - discussion n 11 Nov p 629-30)
Numerical procedures for calculation of stress distribution in sheet-stringer-frame combinations
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 14 , n 8
1947
6 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Diffusion of load in certain sheet-stringer combinations
SLUB | 1938
|Design of hat-type plate-stringer combinations
Engineering Index Backfile | 1944
|