Practical Design of Minimum-Weight Aircraft Structures for Strength and Flutter Requirements
- 1 August 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 13 (8), 614-624
- https://doi.org/10.2514/3.58692
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- A General Method for Flutter OptimizationAIAA Journal, 1973
- Optimization techniques in the structural design processPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- A flutter optimization program for aircraft structural designPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Application of Fully Stressed Design Procedures to Wing and Empennage StructuresJournal of Aircraft, 1971
- Optimization of complex structures to satisfy flutter requirementsAIAA Journal, 1971
- Rates of change of eigenvalues and eigenvectors.AIAA Journal, 1968