Multilevel Optimum Design of Structures with Fiber-Composite Stiffened-Panel Components
- 1 January 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 20 (1) , 138-147
- https://doi.org/10.2514/3.51060
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Simplified direct optimization of tubular truss structuresInternational Journal for Numerical Methods in Engineering, 1981
- MultiLevel Approach to Minimum Weight Deesign Including Buckling ConstraintsAIAA Journal, 1978
- Applications of a Quadratic Extended Interior for Structural Optimization Penalty FunctionAIAA Journal, 1976
- A New Structural Analysis/Synthesis Capability-ACCESS 1AIAA Journal, 1976
- Thin-Walled Elements in Truss SynthesisAIAA Journal, 1973
- A Mixed Optimization Method for Automated Design of Fuselage StructuresJournal of Aircraft, 1972
- Optimized components in truss synthesis.AIAA Journal, 1968