Parametric Constraints with Application to Optimization for Flutter Using a Continuous Flutter Constraint
- 1 April 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 13 (4) , 471-475
- https://doi.org/10.2514/3.49733
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- A comparison of two types of structural optimization procedures for satisfying flutter requirementsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- An Automated Method for Determining the Flutter Velocity and the Matched PointJournal of Aircraft, 1974