Application of Fully Stressed Design Procedures to Wing and Empennage Structures
- 1 September 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 8 (9) , 683-688
- https://doi.org/10.2514/3.59158
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Optimization of structures to satisfy flutter requirements.AIAA Journal, 1969
- A Procedure for Automated Minimum Weight Structural Design: Part I: Theoretical BasisAeronautical Quarterly, 1966
- An integrated approach to structural synthesis and analysisAIAA Journal, 1965