Adaptable Structural Synthesis Using Advanced Analysis and Optimization Coupled by a Computer Operating System
- 1 February 1981
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 18 (2) , 142-149
- https://doi.org/10.2514/3.57475
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- A general panel sizing computer code and its application to composite structural panelsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Preliminary design of composite wings for buckling, strength and displacement constraintsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- A New Structural Analysis/Synthesis Capability-ACCESS 1AIAA Journal, 1976
- On the Accuracy of the Taylor Approximation for Structure ResizingAIAA Journal, 1974