ASOP-3: A Program for Optimum Structural Design to Satisfy Strength and Deflection Constraints
- 1 July 1978
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 15 (7), 422-428
- https://doi.org/10.2514/3.58382
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- ASOP-3 - A program for the optimum design of metallic and composite structures subjected to strength and deflection constraintsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Practical Design of Minimum-Weight Aircraft Structures for Strength and Flutter RequirementsJournal of Aircraft, 1976
- AN ADVANCED STRUCTURAL ANALYSIS/SYNTHESIS CAPABILITY - ACCESSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Optimum design of composite structures with stress and displacement constraintsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- The Quadrilateral ‘Shear’ PanelAircraft Engineering and Aerospace Technology, 1951