Optimum design of composite wing structures by a refined optimality criterion
- 31 December 1991
- journal article
- Published by Elsevier in Composite Structures
- Vol. 17 (1) , 51-65
- https://doi.org/10.1016/0263-8223(91)90060-c
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Optimal design based on optimality criterion for frame structures including buckling constraintComputers & Structures, 1989
- Preliminary Design of Composite Wings for Buckling, Strength, and Displacement ConstraintsJournal of Aircraft, 1979
- Behavior of fully stressed design of structures and its relationshipto minimum-weight design.AIAA Journal, 1965