Comparison of Two Types of Structural Optimization Procedures for Flutter Requirements
- 1 October 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 13 (10) , 1333-1339
- https://doi.org/10.2514/3.60545
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Constrained Structural Optimization for Aeroelastic RequirementsJournal of Aircraft, 1974
- A comparison of two types of structural optimization procedures for satisfying flutter requirementsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Gradient Optimization of Structural Weight for Specified Flutter SpeedJournal of Aircraft, 1974
- A General Method for Flutter OptimizationAIAA Journal, 1973
- A flutter optimization program for aircraft structural designPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Optimization of complex structures to satisfy flutter requirementsAIAA Journal, 1971
- Optimization of structures to satisfy flutter requirements.AIAA Journal, 1969