Preliminary Design of Composite Wings for Buckling, Strength, and Displacement Constraints
- 1 August 1979
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 16 (8) , 564-570
- https://doi.org/10.2514/3.58565
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Applications of a Quadratic Extended Interior for Structural Optimization Penalty FunctionAIAA Journal, 1976
- A New Structural Analysis/Synthesis Capability-ACCESS 1AIAA Journal, 1976
- Structural reanalysis via a mixed methodComputers & Structures, 1975