Optimization of flexible wing structures subject to strength and induced drag constraints
- 1 August 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 15 (8) , 1101-1106
- https://doi.org/10.2514/3.7400
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Applications of a Quadratic Extended Interior for Structural Optimization Penalty FunctionAIAA Journal, 1976
- AEROELASTIC TAILORING OF COMPOSITE MATERIALS TO IMPROVE PERFORMANCEPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- AN ADVANCED STRUCTURAL ANALYSIS/SYNTHESIS CAPABILITY - ACCESSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- OPTIMIZATION OF MULTI-CONSTRAINED STRUCTURES BASED ON OPTIMALITY CRITERIA?Published by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Some Approximation Concepts for Structural SynthesisAIAA Journal, 1974
- Automated Design Optimization of Supersonic Airplane WingStructures under Dynamic ConstraintsJournal of Aircraft, 1973