Effects of structural nonlinearities on limit cycle response of aerodynamic surfaces
- 19 May 1986
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Experimental and Theoretical Study of Nonlinear FlutterJournal of Aircraft, 1981
- = Erträge der Forschung. Bd. 76.Daphnis, 1980