Optimization of structures to satisfy flutter requirements.
- 1 May 1969
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (5), 945-951
- https://doi.org/10.2514/3.5248
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Finite elements applied to panel flutter.AIAA Journal, 1967
- Design of minimum mass structures with specified natural frequencies.AIAA Journal, 1967
- Numerical Solution of Systems of Nonlinear EquationsJournal of the ACM, 1963
- The Calculus of Variations in Applied Aerodynamics and Flight MechanicsPublished by Elsevier ,1962