Optimum design of composite structures with stress and displacement constraints
- 20 January 1975
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Design of optimum structures to impulse type loadingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Optimization of fiber reinforced composite structuresInternational Journal of Solids and Structures, 1973
- A new approach to optimal design of elastic structuresComputer Methods in Applied Mechanics and Engineering, 1973
- Application of Fully Stressed Design Procedures to Wing and Empennage StructuresJournal of Aircraft, 1971
- Design of optimum structuresComputers & Structures, 1971