๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Optimum Design of Laminated Plates under Axial Compression

โœ Scribed by Hirano, Yoichi

Book ID
120232930
Publisher
American Institute of Aeronautics and Astronautics
Year
1979
Tongue
English
Weight
338 KB
Volume
17
Category
Article
ISSN
0001-1452

No coin nor oath required. For personal study only.

๐Ÿ“œ SIMILAR VOLUMES

Design of laminated composite cylindrica
Design of laminated composite cylindrical shells under axial compression
โœ P.M. Weaver ๐Ÿ“‚ Article ๐Ÿ“… 2000 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 545 KB

Approximate expressions describing shape efยฎciency are derived and two charts are shown that help with design. The ยฎrst is a failure chart that shows the complete set of possible designs (and lay-ups) that allow the complexity of the problem to be presented in a simple way. The second is a chart sho

Optimum design of laminated fibre compos
Optimum design of laminated fibre composite plates
โœ L. A. Schmit Jr.; B. Farshi ๐Ÿ“‚ Article ๐Ÿ“… 1977 ๐Ÿ› John Wiley and Sons ๐ŸŒ English โš– 982 KB

## Abstract A method is presented for the minimum weight optimum design of laminated fibre composite plates, subject to multiple inplane loading conditions, which includes stiffness, strength and elastic stability constraints. The buckling analysis is based on an equivalent orthotropic plate approa